UH-1 PDM Sample TO Discrepancy Report (RFP Attch X) DRAFT.xlsx
XLSX spreadsheet 42 KB Posted
- Attached to
- DEPARTMENT OF STATE UH-1 (series) AIRCRAFT PROGRAMMED DEPOT MAINTENANCE (PDM) and H-60 Repairs
- Solicitation number
- 19AQMM22R0006
About this file
This draft solicitation seeks proposals for the Department of State's UH-1 Programmed Depot Maintenance program. Services required include recurring aircraft condition inspections, corrosion identification and repair, component and accessory overhaul, and aircraft refurbishment to ensure high operational availability between maintenance intervals. The solicitation anticipates inducting nine aircraft per year from Peru, Iraq, Uruguay and Panama, with maintenance to be performed in a Central or South American facility if feasible. Interested offerors are requested to submit any comments or questions on the draft statement of work by October 29, 2021.
View the file
Other files
| File | Type | Posted |
|---|---|---|
| Section L DRAFT UH-1 (series) PDM_H-60 (series) Repair DRAFT.docx | DOCX document | |
| UH-1 PDM_H-60 Repair Labor Categories Rates Table (RFP Attch X) DRAFT.xlsx | XLSX spreadsheet | |
| UH-1 PDM_H-60 Repair SOW DRAFT- (RFP 19AQMM22R0006) DRAFT.docx | DOCX document | |
| L M Table UH-1 (series) PDM_H-60 (series) Repair DRAFT.docx | DOCX document | |
| Section M DRAFT UH-1 (series) PDM_H-60 (series) Repair DRAFT.docx | DOCX document | |
| UH-60 Repair Sample TO Discrepancy Report (RFP Attch X) DRAFT.xlsx | XLSX spreadsheet | |
| UH-1 PDM QA Set 3 5-23-22.xlsx | XLSX spreadsheet | |
| QA Set 2.xlsx | XLSX spreadsheet | |
| UH-1 PDM QA Set 1 20220208.xlsx | XLSX spreadsheet | |
| UH-1 PDM SOW DRAFT- 20211014 1253 19AQMM22R0006.docx | DOCX document |
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Text version
135141 Discrep UH-1 Discrepancy List
CRITICAL DISCREPANCIES BELOW
| Seq | Work Required | Corrective Action | Tech Labor Category | Tech Level (I, II, III) | # of Personnel | Base Labor Rate | Man Hours | Burdened Rate | Total |
| 3005 | (6000HR/6YR TBO) Automatic fuel control unit to be overhauled, S/N: B14382. | Mech (Shop) | 20.5 | ||||||
| 4105 | While working Seq 2020, found mast assembly S/N: AFS-53123 to have excessive corrosion and CAD Plating missing on dampers splines. | Mech (Shop) | 12.5 | ||||||
| 4107 | While working Seq 2020, found scissors and sleeve assembly to have scissors arm S/N: EA2444 wrong color. | Mech (Shop) | 6.5 | ||||||
| 4120 | While working Seq 2003, found 42 degree gearbox output quill leaking at seal. | Mech (Shop) | 3.5 | ||||||
| 4121 | While working Seq 2003, found 42 degree gearbox input quill leaking at seal. | Mech (Shop) | 3.5 | ||||||
| 4123 | While working Seq 2003, found 90 degree gearbox input quill leaking at seal. | Mech (Shop) | 3.5 | ||||||
| 17018 | While working Seq 2014, found smartcycle mounting bracket with A5 corrosion through mounting holes. | Mech (Sheet Metal) | 2 | ||||||
| 17038 | While working Seq 2014, found #1 VR base mount hardware has A2 corrosion. | Mech (Sheet Metal) | 1 | ||||||
| 17043 | While working Seq 2014, found AC filter harness chafing smartcycle unit. | Aircraft Mech | 1.75 | ||||||
| 17045 | While working Seq 2014, found pitot drain line chafing drain hose inboard of co-pilot's pedals. | Avionics Tech | 1.25 | ||||||
| 17053 | While working Seq 2014, found relay wires chafing panel 83. | Avionics Tech | 1.25 | ||||||
| 17054 | While working Seq 2014, found wires pinched in clamp through bulkhead between phase adapaters. | Avionics Tech | 1.25 | ||||||
| 17075 | While working Seq 2014, found co-pilot turn slip connector broken. | Avionics Tech | 1.5 | ||||||
| 17076 | While working Seq 2014, found pilot NAT 301 connector screw retainer not installed. | Aircraft Mech | 1 | ||||||
| 17077 | While working Seq 2014, found clamp not installed correctly on bundle below co-pilot cyclic. | Aircraft Mech | 0.75 | ||||||
| 17087 | While working Seq 2014, found terminal board 27 mount hardware and terminal post hardware to have A5 corrosion. | Avionics Tech | 2.5 | ||||||
| 17090 | While working Seq 2014, found KRA 405 radar altimeter mount to have A5 corrosion. | Avionics Tech | 1.75 | ||||||
| 17091 | While working Seq 2014, found rotor brake harness chafing s/w. | Aircraft Mech | 2 | ||||||
| 17093 | While working Seq 2014, found co-pilot wiper harness chafing from connector to circuit breaker panel. | Aircraft Mech | 2 | ||||||
| 17095 | While working Seq 2014, found RPM warning harness chafing shelf. | Avionics Tech | 2 | ||||||
| 17097 | While working Seq 2014, found defrost handle missing decal. | Aircraft Mech | 0.75 | ||||||
| 17098 | While working Seq 2014, found pilot windshield wiper harness chafing at 4 points from connector to circuit breaker panel. | Aircraft Mech | 2.5 | ||||||
| 17100 | While working Seq 2014, found harness chafing heater duct above pilot pedals. | Aircraft Mech | 1.25 | ||||||
| 17101 | While working Seq 2014, found lynx harness chafing ext power wires. | Avionics Tech | 2 | ||||||
| 17113 | While working Seq 2014, found two connectors by crew map light not capped. | Avionics Tech | 0.75 | ||||||
| 17114 | While working Seq 2014, found both mini gun connectors not capped properly. | Aircraft Mech | 1.25 | ||||||
| 17117 | While working Seq 2014, found harness at J96 chafing firewall. | Avionics Tech | 1.25 | ||||||
| 17134 | While working Seq 2014, found harness chafing hydraulic lines inboard and aft of left hand hydraulic disconnect. | Aircraft Mech | 1.25 | ||||||
| 17137 | While working Seq 2014, found ELT has wire pulled out of molex connector. | Avionics Tech | 1 | ||||||
| 17139 | While working Seq 2014, found TDFM lower antenna coax chafing support. | Avionics Tech | 1 | ||||||
| 17142 | While working Seq 2014, found ALE harness chafing heater duct. | Avionics Tech | 1 | ||||||
| 17143 | While working Seq 2014, found HMMS wire chafing bulkhead. | Avionics Tech | 1 | ||||||
| 17146 | While working Seq 2014, found right hand POS light wiring chafing lighting hole. | Avionics Tech | 1 | ||||||
| 17148 | While working Seq 2014, found power feeder harness chafing ICS wires of ELT interface. | Avionics Tech | 1.75 | ||||||
| 17152 | While working Seq 2014, found internal hoist connector not capped and stowed correctly chafing airduct. | Aircraft Mech | 1.25 | ||||||
| 17157 | While working Seq 2014, found ICS harness at right hand side of dome light control chafing power harness for hoist. | Avionics Tech | 1.75 | ||||||
| 17158 | While working Seq 2014, found IVHMMS harness chafing PRC upper coax at terminal board 9. | Avionics Tech | 1.75 | ||||||
| 17159 | While working Seq 2014, found left hand POS light wires chafing lighting hole. | Avionics Tech | 1.25 | ||||||
| 17160 | While working Seq 2014, found ELT coax chafing at antenna. | Avionics Tech | 1.25 | ||||||
| 17163 | While working Seq 2014, found wire broken at debris monitor. | Avionics Tech | 1.5 | ||||||
| 17170 | While working Seq 2014, found terminal board 17 wiring chafing relay K7. | Avionics Tech | 1.25 | ||||||
| 17176 | While working Seq 2014, found wiring from P127 chafing hydraulic line. | Aircraft Mech | 1.25 | ||||||
| 17177 | While working Seq 2014, found qty of 10ea harness clamps from right hand outboard side of hydraulic manifold to transmission oil level light switch deteriorated. | Aircraft Mech | 2.5 | ||||||
| 17179 | While working Seq 2014, found P404 connector rubber oil soaked. | Avionics Tech | 1.5 | ||||||
| 17183 | While working Seq 2014, found J99 rubber oil soaked and deteriorated. | Avionics Tech | 1.5 | ||||||
| 17185 | While working Seq 2014, found tail rotor gearbox HUMMS sensor debonded from gearbox. | Avionics Tech | 1.25 | ||||||
| 17186 | While working Seq 2014, found 42 degree gearbox HUMMS sensor debonded from gearbox. | Avionics Tech | 1.25 | ||||||
| 17187 | While working Seq 2014, found flux valve mounting hardware stripped. | Mech (Shop) | 0.75 | ||||||
| 17194 | While working Seq 2014, found HUMMS harness chafing in 1st forward bulkhead lighting hole. | Avionics Tech | 1.5 | ||||||
| 18034 | While working Seq 2014, found right hand aft c/b faceplate has dead spots. | Avionics Tech | 2 | ||||||
| MAJOR DISCREPANCIES BELOW |
| 13136 | During ACI, found cracked floor support angle in pilot's floor panel at cycle control. | Mech (Sheet Metal) | 6.5 |
| 1025 | Main rotor hub and blade assembly requires removal for ACI Inspection. | Aircraft Mech | 5.5 |
| 1026 | Main rotor blades requires removal for ACI Inspection. | Aircraft Mech | 5.5 |
| 1027 | Mast pole requires removal for ACI Inspection. | Aircraft Mech | 5.5 |
| 1028 | Elevators requires removal for ACI Inspection. | Aircraft Mech | 2.5 |
| 1029 | Stab bar requires removal for ACI inspection. | Aircraft Mech | 5.5 |
| 2025 | Due to historical damage findings when removing riveted down floor panels to FOM all riveted down floor panels are to be removed during initial ACI to inspect for hidden damage to major or minor structural components. | Mech (Sheet Metal) | 65 |
| 2030 | Center engine deck components require removal to facilitate ACI inspection. | Aircraft Mech | 50.5 |
| 2031 | Left hand forward fuel cell requires removal to facilitate ACI inspection. | Aircraft Mech | 10.5 |
| 2032 | Right hand aft fuel cell requires removal to facilitate ACI inspection. | Aircraft Mech | 10.5 |
| 2033 | Left hand aft fuel cell requires removal to facilitate ACI inspection. | Aircraft Mech | 10.5 |
| 2034 | Right hand forward fuel cell requires removal to facilitate ACI inspection. | Aircraft Mech | 10 |
| 2036 | During ACI, found pilot seat armored panel upper bracket damaged and requires replacement. | Aircraft Mech | 1.25 |
| 2041 | During ACI, found co-pilot seat rubber channel deteriorated and requires replacement on all panels. | Aircraft Mech | 5.5 |
| 2042 | During ACI, found pilot seat rubber channel deteriorated and requires replacement on all panels. | Aircraft Mech | 5.5 |
| 2043 | During ACI, found pilot seat bottom cushion deteriorated and requires replacement. | Aircraft Mech | 1.25 |
| 2044 | During ACI, found co-pilot seat bottom cushion deteriorated and requires replacement. | Aircraft Mech | 1.25 |
| 2045 | During ACI, found co-pilot seat back cushion deteriorated and requires replacement. | Aircraft Mech | 1.25 |
| 2046 | During ACI, found pilot seat back cushion deteriorated and requires replacement. | Aircraft Mech | 1.25 |
| 2047 | During ACI, found pilot seat back cover deteriorated and requires replacement. | Aircraft Mech | 2.5 |
| 2048 | During ACI, found co-pilot seat back cover deteriorated and requires replacement. | Aircraft Mech | 2.5 |
| 2049 | During ACI, found co-pilot seat bottom cover out of 24 month life and requires replacement. | Aircraft Mech | 3.5 |
| 2050 | During ACI, found pilot seat bottom cover out of 24 month life and requires replacement. | Aircraft Mech | 3.5 |
| 2051 | During ACI, pilot seat vertical adjustment handle hits frame in lowest setting requiring adjustment. | Aircraft Mech | 1.25 |
| 2052 | During ACI, found co-pilots seat vertical adjustment handle hits frame in lowest setting, requiring adjustment. | Aircraft Mech | 1.25 |
| 2053 | During ACI, found pilot seat vertical adjustment springs stretched and require replacement. | Aircraft Mech | 1.25 |
| 2054 | During ACI, found pilot seat sliding armored panel lock detent requires adjustment. | Aircraft Mech | 1.25 |
| 2055 | During ACI, co-pilot seat sliding armored panel lock detent requires adjustment. | Aircraft Mech | 1.25 |
| 2056 | During ACI, found co-pilot seat shoulder harness runner cracked and requires fabrication and installed of new runner. | Aircraft Mech | 2.5 |
| 2057 | During ACI, found pilot seat shoulder harness runner cracked and requires fabrication and installation of new runner. | Aircraft Mech | 2.5 |
| 2060 | During ACI, found co-pilot seat lap belt out of 5 year life and requires replacement. | Aircraft Mech | 1.25 |
| 2061 | During ACI, found pilot seat lap belt out of 5 year life and requires replacement. | Aircraft Mech | 1.25 |
| 2062 | During ACI, found pilot seat inertia strap out of 5 year life and requires replacement. | Aircraft Mech | 1.25 |
| 2063 | During ACI, found co-pilot seat inertia strap out of 5 year life and requires replacement. | Aircraft Mech | 1.25 |
| 2064 | During ACI, found co-pilot seat shoulder harness out of 5 year life and requires replacement. | Aircraft Mech | 1.25 |
| 2065 | During ACI, found pilot seat shoulder harness out of 5 year life and requires replacement. | Aircraft Mech | 1.25 |
| 2067 | During ACI, found co-pilot seat release handle copper safeties require replacement. | Aircraft Mech | 1.25 |
| 2068 | During ACI, found pilot seat release handle copper safeties require replacement. | Aircraft Mech | 1.25 |
| 2069 | During ACI, found pilot seat ballistic cloth disbonding on all panels and requires replacement. | Aircraft Mech | 30.5 |
| 2071 | During ACI, found co-pilot seat ballistic cloth disbonding on all panels and requires replacement. | Aircraft Mech | 30.5 |
| 2072 | During ACI, found left hand stanchion pole lower mount 6ea rivets loose and require replacement. | Aircraft Mech | 2.5 |
| 2073 | During ACI, found left hand stanchion pole lower quick disconnect inoperable and requires replacement. | Aircraft Mech | 1.25 |
| 2074 | During ACI, found one man without back troop seat cover torn and requires replacement. | Aircraft Mech | 2.5 |
| 2075 | During ACI, found right hand two man with back troop seat cover torn and requires replacement. | Aircraft Mech | 2.5 |
| 2076 | During ACI, found left hand two man with back troop seat cover torn and requires replacement. | Aircraft Mech | 2.5 |
| 2077 | During ACI, found left hand man with back troop seat has damaged legs on frame that require replacement. | Aircraft Mech | 2.5 |
| 2078 | During ACI, found one man without back troop seat has damaged leg on frame that requires replacement. | Aircraft Mech | 1.25 |
| 2079 | During ACI, found one man with back troop seat has damaged back and bottom covers that requires replacement. | Aircraft Mech | 4.5 |
| 2080 | During ACI, found 6ea troop seat belts worn and require replacement. | Aircraft Mech | 1.75 |
| 2081 | During ACI, found 2ea seat mounts on forward pylon panel damaged and require replacement. | Aircraft Mech | 2.5 |
| 2083 | During ACI, found co-pilot airframe and door seals torn requiring replacement. | Mech (Shop) | 12.5 |
| 2084 | During ACI, found pilot airframe and door seals torn requiring replacement. | Mech (Shop) | 12.5 |
| 2085 | During ACI, found left hand and right hand heavy duty skids with multiple cracks on bottom side requiring replacement. | Aircraft Mech | 5.5 |
| 2086 | During ACI, found pilot cyclic boot has A5 corrosion in retaining strap. | Aircraft Mech | 0.75 |
| 2087 | During ACI, found co-pilot cyclic boot has holes in it. | Aircraft Mech | 0.75 |
| 2088 | During ACI, found 2ea forward landing gear caps rubber cracked and de-bonding, requiring replacement. | Mech (Shop) | 6.5 |
| 2089 | During ACI, found pilot collective boot torn and zipper broken. | Aircraft Mech | 0.75 |
| 2090 | During ACI, found co-pilot collective boot with A5 corrosion in retaining strap. | Aircraft Mech | 0.75 |
| 2091 | During ACI, found Tee fitting to J-line corroded and damaged threads. (Fig 2-5-6 #41) | Aircraft Mech | 1.25 |
| 2092 | During ACI, found left hand and right hand forward loop line seals deteriorated. | Aircraft Mech | 1.25 |
| 2093 | During ACI, found 3ea rollover valve gaskets deteriorated. | Aircraft Mech | 4.25 |
| 2094 | During ACI, found nut retainer on right hand fuel sump drain valve with A5 corrosion. | Aircraft Mech | 0.75 |
| 2095 | During ACI, found left hand and right hand upper cargo door seals torn requiring replacement. | Mech (Shop) | 5.5 |
| 2097 | During ACI, found left hand and right hand forward cargo door seals torn requiring replacement. | Mech (Shop) | 5.5 |
| 2098 | During ACI, found left hand and right hand aft and forward jump door seals torn requiring replacement. | Mech (Shop) | 5.5 |
| 2099 | During ACI, found left hand and right hand upper and lower door seals torn requiring replacement. | Mech (Shop) | 5.5 |
| 2100 | Transcribed from 2408-13-1, right hand landing gear cap rubber de-bonding on outboard side aft crosstube (repair or replace next 90 day cci) | Mech (Shop) | 3.5 |
| 2101 | Transcribed from 2408-13-1, left hand landing gear cap rubber split on outboard side aft crosstube (replace next 90 day cci). | Mech (Shop) | 3.5 |
| 2102 | During ACI, found left hand aft fuel cell has blisters and delamination. | Aircraft Mech | 30.5 |
| 2103 | During ACI, found right hand forward fuel cell has blisters and baffle torn on inside. | Aircraft Mech | 30.5 |
| 2104 | During ACI, found tail rotor servo clevis with A5 corrosion and pitting. | Aircraft Mech | 1.75 |
| 2105 | During ACI, found tail rotor bellcrank P/N: 212-001-711-1 with 2ea bad bearings. | Aircraft Mech | 10 |
| 2106 | During ACI, found left hand and right hand fuel cell vent valves with mechanical damage. | Aircraft Mech | 0.75 |
| 2107 | During ACI, found flapper valve cracked in right hand forward fuel cell. | Aircraft Mech | 2.5 |
| 2108 | During ACI, found flapper valve cracked in left hand forward fuel cell. | Aircraft Mech | 2.5 |
| 2109 | During ACI, found left hand forward fuel cell has blisters and delamination on inside. | Aircraft Mech | 31 |
| 2110 | During ACI, found crossover fuel line, P/N: AE7013075K0121 both fittings corroded and deteriorated inside. | Aircraft Mech | 1.25 |
| 2111 | During ACI, found flapper valve plates cracked around mount holes in right hand forward fuel cell. | Aircraft Mech | 0.75 |
| 2112 | During ACI, found crossover fuel line, P/N: AE7013075K0096 both fitting corroded and deteriorated inside. | Aircraft Mech | 1.25 |
| 2113 | During ACI, found drain valve on right hand forward fuel cell with A5 corrosion. | Aircraft Mech | 0.75 |
| 2114 | During ACI found nut retainer for drain valve on right hand forward fuel cell with A5 corrosion. | Aircraft Mech | 0.75 |
| 2115 | During ACI, found left hand forward fuel cell access cover to have pitting and corrosion in O-ring groove. | Aircraft Mech | 0.75 |
| 2116 | During ACI, found nut retainer for drain on left hand fuel sump with A5 corrosion. | Aircraft Mech | 1.25 |
| 2117 | During ACI, found ejector pump support cracked in right hand forward fuel cell. | Aircraft Mech | 0.75 |
| 2118 | During ACI, found center fuel cell has blisters and delamination. | Aircraft Mech | 31 |
| 2119 | During ACI, found right hand aft fuel cell has blisters and delamination. | Aircraft Mech | 31 |
| 2120 | During ACI, found valve on left hand fuel sump safety wire holes damaged. | Aircraft Mech | 1.25 |
| 2121 | During ACI, found lift link upper and lower bolts bushing debonded from bolt requiring replacement. | Aircraft Mech | 0.75 |
| 2122 | During ACI, found lift link damaged, no damage allowed on outer 2.5 inches of link IAW Bell 212 CR&O Fig 63-113. | Aircraft Mech | 0.75 |
| 2123 | During ACI, found 2ea transmission mount boots torn. | Aircraft Mech | 0 |
| 2126 | During ACI, found 4ea candlesticks with mechanical damage on both ends no damage allowed on threaded end IAW BHT-212-CR&O Fig 63-114. | Aircraft Mech | 0 |
| 2127 | During ACI, found 2ea friction dampers with mechanical damage around bearings requiring replacement. | Aircraft Mech | 0 |
| 2128 | During ACI, found 4ea transmission mounts with A5 corrosion around mount holes requiring replacement. | Aircraft Mech | 0 |
| 2129 | During ACI, found right hand cyclic servo control tube universal bearing ratcheting and worn. | Aircraft Mech | 0 |
| 2130 | During ACI, found left hand cyclic servo clevis lock broken. | Aircraft Mech | 0 |
| 2131 | During ACI, found left hand cyclic servo control tube universal bearing ratcheting and worn. | Aircraft Mech | 0 |
| 2132 | During ACI, found collective servo control tube universal bearing ratcheting and worn. | Aircraft Mech | 0 |
| 2133 | During ACI, found right hand cyclic servo clevis lock broken. | Aircraft Mech | 0 |
| 2134 | During ACI, found fuel line P/N: 212-061-606-1 kinked in radius. | Aircraft Mech | 1.25 |
| 2135 | During ACI, found fuel line P/N: 212-061-613-1 with dents in radius. | Aircraft Mech | 1.25 |
| 2136 | During ACI, found oil cooler and lines require disassembly from cowling to accommodate sheetmetal repairs. | Aircraft Mech | 7.5 |
| 2137 | During ACI, found fuel line P/N: AE7010100K0171 fittings corroded and deteriorated on inside. | Aircraft Mech | 1.25 |
| 2138 | During ACI, found fuel J line P/N: AE7010200K0056 with multiple steel strands broken. | Aircraft Mech | 1.25 |
| 2139 | During ACI, found fuel line P/N: AE7010030N0126 fittings corroded and deteriorated on inside. | Aircraft Mech | 1.25 |
| 2140 | During ACI, found fuel line P/N: AE7010000K0292 fittings corroded and deteriorated on inside. | Aircraft Mech | 1.25 |
| 2141 | During ACI, found fuel line P/N: 212-061-644-1 corroded and several steel strands broken. | Aircraft Mech | 1.25 |
| 2142 | During ACI, found fuel line P/N: 212-061-646-1 corroded and several steel strands broken. | Aircraft Mech | 1.25 |
| 2143 | During ACI, found hydraulic system pump splines worn and pitted. | Aircraft Mech | 1.25 |
| 2144 | During ACI, found tail rotor control tube P/N: 212-001-056-1 cracked at bearing housing. | Aircraft Mech | 1.25 |
| 2145 | During ACI, found left hand and right hand hanger bearing support legs with elongated holes and A5 corrosion in mount holes. | Aircraft Mech | 0 |
| 2146 | During ACI, found #1 hanger bearing support with elongated holes and A5 corrosion in mount holes. | Aircraft Mech | 0 |
| 2148 | During ACI, found right hand vent plenum in nose missing clamps around ducts. | Aircraft Mech | 3.5 |
| 2149 | During ACI, found pilot seat tracks to be ribbed and have elongated holes and require replacement. | Aircraft Mech | 3.5 |
| 2150 | During ACI, found co-pilot seat tracks to be ribbed and to have elongated holes and requires replacement. | Aircraft Mech | 4.5 |
| 2153 | During ACI, found co-pilot collective #1 and #2 throttle grips deteriorated. | Aircraft Mech | 7.5 |
| 2154 | During ACI, found collective failed minimum friction pull check. | Aircraft Mech | 12.5 |
| 2156 | During ACI, found left hand and right hand wiper blades cracked and deteriorated. | Aircraft Mech | 1.75 |
| 2158 | During ACI, found fuel line, P/N: AE7010000K0114, with several broken strands and corrosion inside fitting. | Aircraft Mech | 2.5 |
| 2159 | During ACI, found fuel coupling, P/N: 205-062-652-1, with A5 corrosion. | Aircraft Mech | 2.5 |
| 2163 | During ACI, found left hand cyclic bellcrank, P/N: 212-001-312-1, has 3ea bad bearings. | Mech (Shop) | 11.5 |
| 2164 | During ACI, found right hand cyclic bellcrank, P/N: 212-001-312-1, has 3ea bad bearings. | Mech (Shop) | 12 |
| 2165 | During ACI, found left hand and right hand wiper arm failed pull check. | Aircraft Mech | 3.25 |
| 2166 | Transcribed from 2408-13-1, engine control jackshaft #1 engine shaft spacer is worn. | Aircraft Mech | 5.5 |
| 2167 | During ACI, found right hand fuel breakaway valve with mechanical damage and A5 corrosion. | Aircraft Mech | 1.25 |
| 2168 | During ACI, found center fuel cell probe wire frayed and connectors with corrosion. | Aircraft Mech | 1.25 |
| 2170 | During ACI, found tube assembly in left hand AVI compartment with several sharp dents. | Avionics Tech | 1.25 |
| 2171 | During ACI, found left hand fuel breakaway valve with mechanical damage with A5 corrosion. | Aircraft Mech | 1.25 |
| 2173 | During ACI, found panel 10 combining gearbox panel seals torn, requiring replacement. | Mech (Shop) | 4.5 |
| 2174 | During ACI, found left hand outboard induction baffle seals torn/oil soaked, requiring replacement. | Mech (Shop) | 4 |
| 2175 | During ACI, found right hand outboard induction baffle seals torn/oil soaked, requiring replacement. | Mech (Shop) | 4 |
| 2176 | During ACI, found left hand lower swing cowling seals are missing. | Mech (Shop) | 4.5 |
| 2178 | During ACI, found oil cooler air scoop left hand cowling seals deteriorated, requiring replacement. | Mech (Shop) | 3.5 |
| 2179 | During ACI, found right hand lower induction baffle has 3ea seals torn/oil soaked, requiring replacement. | Mech (Shop) | 3.5 |
| 2180 | During ACI, found left hand lower induction baffle has all seals torn/oil soaked, requiring replacement. | Mech (Shop) | 4 |
| 2181 | During ACI, found 2ea front monopod mounts with bad bearings. | Mech (Shop) | 10.5 |
| 2182 | During ACI, found right hand outboard induction baffle seals torn, requiring replacement. | Mech (Shop) | 3.5 |
| 2183 | During ACI, found P/N: 212-001-710-1, bellcrank with 3ea bad bearings. | Mech (Shop) | 8.5 |
| 2184 | During ACI, found 10ea sets of tail rotor driveshaft clamps with grooves worn in radius and mechanical damage around bolt holes. | Aircraft Mech | 0 |
| 2185 | During ACI, found co-pilot chin bubble crazed, STA20 WL20 BL30 | Mech (Shop) | 40.5 |
| 2186 | During ACI, found pilot chin bubble has scratchers that would obstruct pilot view IAW DOS INL/A TM 1-UH-1ST-23 Fig 2-2. | Mech (Shop) | 40.5 |
| 2187 | During ACI, found co-pilot door forward window has scratchers that obstruct pilot view IAW DOS INL/A TM 1-UH-1ST-23 Fig 2-2. | Mech (Shop) | 10.5 |
| 2188 | During ACI, found co-pilot door sliding window crazed, STA42 WL38 BL37L, IAW DOS INL/A TM 1-UH-1ST-23 Fig 2-2.-- | Mech (Shop) | 4.5 |
| 2189 | During ACI, found co-pilot door upper window cracked, STA42 WL69 BL37L, IAW DOS INL/A 1-UH-1ST-23 Fig 2-2. | Mech (Shop) | 4.5 |
| 2190 | During ACI, found co-pilot greenhouse has scratches that would obstruct pilot view, STA45 WL71 BL30, IAW DOS INL/A TM 1-UH-1ST-23 Fig 2-2. | Mech (Shop) | 30.5 |
| 2191 | During ACI, found co-pilot windshield delaminated, STA33 WL70 BL14L, IAW DOS INL/A TM 1-UH-1ST-23 Fig 2-2. | Mech (Shop) | 40.5 |
| 2192 | During ACI, found pilot door upper window has scratches that obstruct pilot view, STA42 WL69 BL37R, IAW INL/A TM 1-UH-1ST-23 Fig 2-2. | Mech (Shop) | 4.5 |
| 2193 | During ACI, found pilot greenhouse has scratches that would obstruct pilot view, STA45 WL71 BL30R, IAW DOS INL/A TM 1-UH-1ST-23 Fig 2-2. | Mech (Shop) | 30.5 |
| 2194 | During ACI, found pilot door sliding window has scratches that obstruct pilot view, STA42 WL38 BL37R, IAW DOS INL/A TM 1-UH-1ST-23 Fig 2-2. | Mech (Shop) | 4.5 |
| 2195 | During ACI, found pilot windshield delaminated, STA33 WL70 BL14R, IAW DOS INL/A TM 1-UH-1ST-23 Fig 2-2.3. | Mech (Shop) | 40.5 |
| 2196 | During ACI, found right hand jump door window has scratches that obstruct crew view, STA74 WL38 BL38R, IAW DOS INL/A TM 1-UH-1ST-23 Fig 2-2. | Mech (Shop) | 10.5 |
| 2197 | During ACI, found left hand forward upper door track worn beyond limits, STA75 WL72 BL41L, IAW DOS INL/A TM 1-UH-1ST-23 Fig 2-16.2. | Mech (Shop) | 30.5 |
| 2198 | During ACI, found right hand forward upper door track worn beyond limits, STA75 WL72 BL41R, IAW DOS INL/A TM 1-UH-1ST-23 Fig 2-16.2. | Mech (Shop) | 30.5 |
| 2199 | During ACI, found left hand forward lower door track worn beyond limits, STA75 WL22 BL41L, IAW DOS INL/A TM 1-UH-1ST-23 Fig 2-16.2. | Mech (Shop) | 30.5 |
| 2200 | During ACI, found left hand aft lower door track worn beyond limits, STA156 WL36 BL30L, IAW DOS INL/A TM 1-UH-1ST-23 Fig 2-16.2. | Mech (Shop) | 30.5 |
| 3000 | Main rotor blades to be sent to vendor for evaluation, paint, and balancing per DoS. | Supply Tech | 4 |
| 3001 | Engine removed to send to vendor for evaluation, per contract requirements. | Supply Tech | 0 |
| 3002 | Prep and ship main rotor blades. | Supply Tech | 6 |
| 3003 | Engine requires removal of all QCA components prior to shipping engine to vendor. | Mech (Shop) | 40 |
| 3004 | Install engine QCA | Mech (Shop) | 40 |
| 3006 | UH-1ST-INSP-019, 1000 hours or 12 months special inspection of main rotor blades due in reference to DOS INL/A TM 1-UH-1ST-23. | Aircraft Mech (QA) | 3 |
| 4001 | Mast pole assembly removed by customer and requires installation. | Aircraft Mech | 4 |
| 4002 | While working Seq 3003, found main driveshaft adapter lock washer damaged beyond serviceable limits. | Aircraft Mech | 2.5 |
| 4012 | UH-1ST-AD-15-02, inspect tail rotor blades for cracks and damage using a 3X and 10X magnifying glass in reference to AD2013-15-02, ASB212-13-147, & QCL13-119. | Mech (Shop) | 2.5 |
| 4013 | UH-1ST-ASB-212-00-107, inspect tail rotor counterweight bellcrank retention nut and CPC coating for condition and security IAW ASB-212-00-107 & QCL13-097. | Mech (Shop) | 1.25 |
| 4031 | UH-1ST-INSP-022, 24 month removal and inspection of flight control system bolts, refer to Chap 4 for retirement life of rotating control bolts due in reference to DOS INL/A TM 1-UH-1ST-23. | Mech (Shop) | 24.5 |
| 4032 | UH-1ST-INSP-818, 10 hour one time recurring 25 hour inspection of main rotor grip using a 10X magnifying glass required in reference to Aircraft MM, Chap 1 Special Inspections, AD2013-13-06 & QCL13-125. | Mech (Shop) | 2.5 |
| 4033 | UH-1ST-ASB-212-08-130, one time inspection and recurring inspection of main rotor blade, P/N 212-015-501-005, -111, -113, -115, -117, -119, & -121, 204-012-001-023, and -033 and 210-015-001-101 in reference to BHT-ASB-212-08-130 Revision C and AD2012 | Mech (Shop) | 1.25 |
| 4034 | UH-1ST-INSP-087, perform a 100 hour/12 month visual inspection of transmission main case, P/N 204-040-353-023, just above main input quill (fluorescent penetrant for cases that have webbing removed or re-worked) in reference to Dyncorp Memorandum QCL | Mech (Shop) | 2.5 |
| 4045 | UH-1ST-INSP-007A, 12 month/600 hour visual inspection and lubrication of tail rotor driveshaft flexible couplings due in reference to DOS INL/A TM 1-UH-1St-23 & QCM10-033. | Mech (Shop) | 16.5 |
| 4046 | Comply with QCL21-063, main rotor mast assembly upgrade. | Mech (Shop) | 5.5 |
| 4047 | H-II-INSP-081 1200 HR/24 month inspection of main rotor grips with buffer pad installed on inner surface of blade bolt tangs required Ref AD 2013-13-06 & QCL 13-125. | Mech (Shop) | 2 |
| 4048 | While working Seq 2020, found both dampers, white S/N: UVC7612 and red S/N: R201851, levers and adapters with multiple paint layers and areas of bare metal. | Mech (Shop) | 10.5 |
| 4049 | While working Seq 2020, found red damper S/N: R201851 with dirty fluid and dirty inspection window causing verification of correct timing pin movement impossible. | Mech (Shop) | 6.5 |
| 4050 | While working Seq 2020, found white damper S/N: UVC7612 with dirty fluid and dirty inspection window causing verification of correct timing pin movement impossible. | Mech (Shop) | 6.5 |
| 4051 | While working Seq 2020, found stabilizer bar assembly S/N: A-955, requires complete disassembly for inspection and reassembly. | Mech (Shop) | 8.5 |
| 4052 | While working Seq 2020, found stabilizer bar assembly S/N: A-955 and it's components with multiple layers of paint and bare metal in spots and multiple colors. | Mech (Shop) | 12.5 |
| 4055 | While working Seq 2020, found red stab-bar mixing lever, S/N: RE10725, with 1ea outboard bearing ratcheting and flat spots. | Mech (Shop) | 5.5 |
| 4056 | While working Seq 2020, found white stab-bar mixing lever, S/N: RE10688 with 1ea outboard bearing ratcheting, flat spots and dust shield missing. | Mech (Shop) | 5.5 |
| 4057 | While working Seq 2020, found white stab-bar mixing lever, S/N: RE10688 with 2ea inboard bearings with ratcheting/rough travel and damaged dust shield. | Mech (Shop) | 3.5 |
| 4058 | While working Seq 2007, found tail rotor output 1ea coupling, P/N: 204-040-604-005 S/N: A-FS62841 and 1ea coupling, P/N: 204-040-603-009 S/N: 3911, to have loss of CAD plating. | Mech (Shop) | 1.5 |
| 4059 | While working Seq 2007, found transmission support case 4ea washers P/N: 204-040-736-001 and 4ea washers P/N: 204-040-236-001 to have loss of CAD plating. | Mech (Shop) | 3.5 |
| 4060 | While working Seq 2020, found red stab-bar mixing lever S/N: RE10725, with 2ea inboard bearings ratcheting/rough travel and flat spots. | Mech (Shop) | 3.5 |
| 4061 | While working Seq 2020, found both the red and white main rotor pitch link barrel assemblies with approximately .001 mechanical damage // max allowed .010. | Mech (Shop) | 3.5 |
| 4062 | While working Seq 2020, found both pitch change link universal bearings binding, ratcheting and rough travel. | Mech (Shop) | 4.5 |
| 4063 | While working Seq 2007, found hydraulic quill seals shows evidence of leaking. | Mech (Shop) | 4.5 |
| 4064 | While working Seq 2007, found elevator support bellcrank bearings have excessive play. | Mech (Shop) | 3.5 |
| 4065 | While working Seq 2007, found elevator support bellcrank ratcheting. | Mech (Shop) | 3.5 |
| 4068 | While working Seq 2007, found tail rotor output seal shows evidence of leaking. | Mech (Shop) | 2.5 |
| 4069 | While working Seq 2007, found that seal shows evidence of leaking on hydraulic pump quill. | Mech (Shop) | 3 |
| 4070 | 42 Degree gearbox input couplings have loss of CAD-Plating. | Mech (Shop) | 0 |
| 4071 | 42 Degree gearbox output couplings have loss of CAD-Plating. | Mech (Shop) | 0 |
| 4072 | Tail rotor gearbox couplings have loss of CAD-Plating. | Mech (Shop) | 0 |
| 4073 | While working Seq 2006, found tail rotor hub and blade assembly, S/N: PSD272 will require a static balance after reassembly. | Mech (Shop) | 4.5 |
| 4074 | While working Seq 2006, found tail rotor hub and blade assembly, S/N: PSD143 requires disassembly. | Mech (Shop) | 8.5 |
| 4075 | While working Seq 2006, found tail rotor hub and blade assembly, S/N: PSD143 and components have areas of bare metal and incorrect color for current configuration. | Mech (Shop) | 9.5 |
| 4076 | While working Seq 2006, found white tail rotor blade, S/N: A-12617 with leading and trailing edge erosion, paint flaking at bolt holes and areas of bare metal. | Mech (Shop) | 8.5 |
| 4077 | While working Seq 2020, found both stabilizer bar center frame support pivot bearing sets with flat spots and dust shield retaining clips missing. | Mech (Shop) | 4.5 |
| 4078 | While working Seq 2020, found both stabilizer bar center frame support pivot bearing retaining plates with .002 mechanical damage. | Mech (Shop) | 2.5 |
| 4079 | While working Seq 2020, found white stab-bar mixing lever, S/N: RE10688 with mechanical damage approximately .003 on the inboard side of lever // max allowed .035 and .002 at universal bearing attachment point // max allowed .010. | Mech (Shop) | 2.5 |
| 4080 | While working Seq 2020, found both stab-bar center frame supports with approximately .002 mechanical damage // max allowed .035. | Mech (Shop) | 3.5 |
| 4081 | While working Seq 2020, found 1ea stabilizer bar center frame support pivot bearing bolt scoured and pitted. | Mech (Shop) | 1.25 |
| 4085 | While working Seq 2010, found left hand oil/fuel heater hose fire sleeve is too short. | Mech (Shop) | 3.5 |
| 4086 | While working Seq 2020, found 2ea aft engine mount bearings with excessive play. | Mech (Shop) | 2.5 |
| 4087 | While working Seq 2010, found #1 starter 4 inch brush sets worn beyond serviceable limits. | Mech (Shop) | 3.5 |
| 4088 | #2 Hanger bearing couplings have loss of CAD-Plating. | Mech (Shop) | 0 |
| 4089 | #1 Hanger bearing couplings have loss of CAD-Plating. | Mech (Shop) | 0 |
| 4092 | While working Seq 2006, found tail rotor crosshead assembly requires disassembly. | Mech (Shop) | 6.5 |
| 4093 | While working Seq 2006, found the tail rotor crosshead assembly and its components all with areas of bare metal, missing and flaking paint. | Mech (Shop) | 7.5 |
| 4094 | While working Seq 2006, found the tail rotor crosshead assembly with intergranular corrosion, missing cadnium plating and bellcrank spindles have fretting. | Mech (Shop) | 4.5 |
| 4095 | While working Seq 2006, inspection found the tail rotor crosshead assembly retaining nut with intergranular corrosion and missing cadnium plating. | Mech (Shop) | 4.5 |
| 4096 | While working Seq 2006, found fifth mount with paint flaking in several locations and areas of bare metal. | Mech (Shop) | 7.5 |
| 4097 | While working Seq 2006, found fifth mount has corrosion. | Mech (Shop) | 2.5 |
| MINOR DISCREPANCIES BELOW |
| 2037 | During ACI, found co-pilot seat warning stencil on back of seat requires painting. | Aircraft Mech | 1 |
| 2038 | During ACI, found pilot seat warning stencil on back on seat requires painting. | Aircraft Mech | 1 |
| 2039 | During ACI, found pilot seat has areas of bare metal on frame that require paint. | Aircraft Mech | 2 |
| 2040 | During ACI, found co-pilot seat has areas of bare metal on frame that require paint. | Aircraft Mech | 2 |
| 2058 | During ACI, found pilot seat insert assembly has areas of bare metal and requires paint. | Aircraft Mech | 2.5 |
| 2059 | During ACI, found co-pilot seat insert assembly has areas of bare metal and requires paint. | Aircraft Mech | 2 |
| 2066 | During ACI, found pilot seat vertical adjustment slides requires cleaning and lubrication. | Aircraft Mech | 1 |
| 2070 | During ACI, found co-pilot seat vertical adjustment slides requires cleaning and lubrication. | Aircraft Mech | 1 |
| 2096 | During ACI, found left hand and right hand 166 bulkhead seals torn requiring replacement. | Mech (Shop) | 7 |
| 2124 | During ACI, found 5ea transmission mount bushings requiring touch up paint. | Mech (Shop) | 1 |
| 2125 | During ACI, found 4ea transmission spacers require primer. | Aircraft Mech | 1 |
| 2147 | During ACI, found tailboom seal torn requiring replacement. | Aircraft Mech | 2 |
| 2151 | During ACI, found pilot's door lower hinge has 1ea rusty/corroded screw and springs. | Aircraft Mech | 1.5 |
| 2152 | During ACI, found pilot's door upper hinge has rusty/corroded spring leafs and 2ea screws. | Aircraft Mech | 1.5 |
| 2155 | During ACI, found pitot cover torn. | Avionics Tech | 0.25 |
| 2157 | During ACI, found left hand and right hand cargo door retainers cracked. | Mech (Sheet Metal) | 0.5 |
| 2160 | During ACI, found 10ea clamps in hellhole oil soaked and torn. | Aircraft Mech | 5 |
| 2161 | During ACI, found 13ea clamps in forward hydraulic panel oil soaked and torn. | Aircraft Mech | 5 |
| 2162 | During ACI, found left hand and right hand cargo door stop bumpers deteriorated. | Aircraft Mech | 6 |
| 2169 | During ACI, found 5ea drain tubes for engine deck clamps, oil soaked and torn. | Aircraft Mech | 4 |
| 2177 | During ACI, found right hand lower swing cowling upper seal is missing. | Aircraft Mech | 3 |
| 4003 | While working Seq 3003, found engine mount bearings worn beyond serviceable and repairable limits. | Mech (Shop) | 2 |
| 4004 | While working Seq 3003, found jackshaft rod damaged beyond serviceable and repairable limits. | Mech (Shop) | 2 |
| 4005 | While working Seq 3003, found metallic vent hose (c-box, top center) damaged beyond serviceable limits. | Mech (Shop) | 2 |
| 4006 | While working Seq 3003, found primer on jackshaft tube assembly, qty 2ea damaged beyond servieable limits. | Mech (Shop) | 5 |
| 4053 | While working Seq 2020, found stabilizer bar assembly S/N: A-955 has approximately .002 mechanical damage around the mixing lever areas and on the outer tubes. | Mech (Shop) | 2 |
| 4054 | While working Seq 2020, found red stab-bar mixing lever, S/N: RE10725 with mechanical damage approximately .002 on the inboard side of lever // max allowed .035 and .002 at universal bearing attachment point // max allowed .010. | Mech (Shop) | 2 |
| 4067 | While working Seq 2007, found transmission drain tubing clamps oil soaked and worn. | Mech (Shop) | 1 |
| 4082 | While working Seq 2020, found red scissor control tube, S/N: A-FS5355 with mechanical damage approximately .002 end of tube assembly // max allowed .005. | Mech (Shop) | 2 |
| 4083 | While working Seq 2020, found white scissor control tube, S/N: A-FS6804 with mechanical damage approximately .002 end of tube assembly // max allowed .005. | Mech (Shop) | 2 |
| 4084 | While working Seq 2020, found 4ea scissor control tube rubber bumper washers torn and incorrect size. | Mech (Shop) | 2 |
| 4091 | While working Seq 2020, inspection found all hardware for both damper assemblies and components with excessive corrosion. | Mech (Shop) | 1.75 |
| 4109 | While working Seq 2020, found mast boot spacer torn. | Mech (Shop) | 1.75 |
| 4110 | While working Seq 2020, found collective levers spacer to have corrosion inside. | Mech (Shop) | 1.5 |
| 4111 | While working Seq 2020, found collective lever S/N: REFS 1515 to have corrosion at spacer area. | Mech (Shop) | 1.5 |
| 4112 | While working Seq 2020, found collective lever S/N REFS 1464 to have corrosion at spacer area. | Mech (Shop) | 1.5 |
| 13177 | During ACI, found forward transmission firewall seals are deteriorated and oil soaked, requires replacement. | Mech (Shop) | 6 |
| 17019 | While working Seq 2014, found clamp hardware forward of right hand ALE 47 sensor connector with A1 corrosion. | Aircraft Mech | 0.75 |
| 17020 | While working Seq 2014, found ground stud hardware inboard of and below transistor in the nose with A5 corrosion. | Aircraft Mech | 0.75 |
| 17021 | While working Seq 2014, found right hand forward AAR-47 sensor connector not capped properly. | Avionics Tech | 0.75 |
| 17022 | While working Seq 2014, found left hand forward AAR-47 sensor connector not capped properly. | Avionics Tech | 0.75 |
| 17023 | While working Seq 2014, found KG102 mount base hardware with A5 corrosion. | Aircraft Mech | 1 |
| 17024 | While working Seq 2014, found clamp hardware forward of left hand AAR 47 sensor connector with A1 corrosion. | Avionics Tech | 0.75 |
| 17025 | While working Seq 2014, found MD1 gyro mount hardware has A5 corrosion. | Avionics Tech | 1 |
| 17026 | While working Seq 2014, found harness clamp hardware through upper nose shelf outboard of #2 VR has A5 corrosion. | Aircraft Mech | 1 |
| 17027 | While working Seq 2014, found right hand vent blower capacitor housing with A5 corrosion. | Aircraft Mech | 0.75 |
| 17028 | While working Seq 2014, found bonding strap mount hardware for right hand vent blower capacitor to have A5 corrosion. | Aircraft Mech | 1 |
| 17029 | While working Seq 2014, found smartcycle mount plate hardware corroded. | Aircraft Mech | 1 |
| 17030 | While working Seq 2014, found upper nose shelf MAI bundle center large clamp hardware to have A5 corrosion. | Aircraft Mech | 0.75 |
| 17031 | While working Seq 2014, found 2ea clamps and hardware on pitot line above main bundle and switching units have A5 corrosion. | Avionics Tech | 1 |
| 17032 | While working Seq 2014, found #2 voltage reg base mount hardware to have A5 corrosion. | Avionics Tech | 0.75 |
| 17033 | While working Seq 2014, found battery tie down rods has A5 corrosion at base. | Avionics Tech | 0.75 |
| 17034 | While working Seq 2014, found battery tie down rods wingnuts and bracket with A5 corrosion. | Avionics Tech | 0.75 |
| 17035 | While working Seq 2014, found power supply inboard and below transistors in the nose case with A2 corrosion. | Avionics Tech | 0.75 |
| 17036 | While working Seq 2014, found 2 mount screws on TB 62-64 rack to have A2 corrosion. | Avionics Tech | 0.75 |
| 17037 | While working Seq 2014, found #1 VR and base latch point have A1 corrosion. | Avionics Tech | 0.75 |
| 17039 | While working Seq 2014, found saddle clamp hardware on all 4 switching units with A2 corrosion. | Avionics Tech | 0.75 |
| 17040 | While working Seq 2014, found RAD ALT R/T connector missing seal pins. | Avionics Tech | 0.75 |
| 17041 | While working Seq 2014, found KA 138 relay to have A2 corrosion. | Avionics Tech | 1.25 |
| 17042 | While working Seq 2014, found KTR 909 mount to have A5 corrosion. | Avionics Tech | 1.5 |
| 17044 | While working Seq 2014, found screws on power supply below nose transistors have no thread protrusion. | Avionics Tech | 1 |
| 17046 | While working Seq 2014, found A1 corrosion around base of 5 ground stud stations inboard of KRA 405B. | Avionics Tech | 1.25 |
| 17047 | While working Seq 2014, found harness clamp and hardware through upper nose shelf outboard of #1 VR to have A5 corrosion. | Avionics Tech | 1.5 |
| 17048 | While working Seq 2014, found ground stud outboard of #1 vent blower to have A5 corrosion. | Avionics Tech | 1 |
| 17049 | While working Seq 2014, found bonding strap mount hardware for left hand vent blower capacitor to have A5 corrosion. | Avionics Tech | 1 |
| 17050 | While working Seq 2014, found K9 relay boot torn. | Avionics Tech | 0.75 |
| 17055 | While working Seq 2014, found test points beside aircraft battery hardware with A1 corrosion. | Avionics Tech | 0.75 |
| 17058 | While working Seq 2014, found transmission oil level light circuit breaker forward and below pilot pedal amp unreadable. | Avionics Tech | 1.25 |
| 17060 | While working Seq 2014, found 4 screws on 1st and 2nd row of circuit breakers have A5 corrosion. | Avionics Tech | 0.75 |
| 17061 | While working Seq 2014, found P122 backshell not installed. | Avionics Tech | 1.25 |
| 17062 | While working Seq 2014, found spare lamp holder small bulbs painted and rubber inserts deteriorated. | Avionics Tech | 1 |
| 17063 | While working Seq 2014, found co-pilot ICS connector wiring deteriorated at terminal board 22. | Avionics Tech | 1.25 |
| 17064 | While working Seq 2014, found pilot map light TB terminal hardware corroded. | Avionics Tech | 1.25 |
| 17065 | While working Seq 2014, found co-pilot map light TB mount hardware corroded. | Avionics Tech | 1.25 |
| 17066 | While working Seq 2014, found co-pilot map light ground stud corroded. | Avionics Tech | 1.25 |
| 17067 | While working Seq 2014, found pilot ICS connector wiring deteriorated at terminal board 23. | Avionics Tech | 1.25 |
| 17068 | While working Seq 2014, found corroded ground stud hardware inboard of terminal board 23. | Avionics Tech | 1.25 |
| 17069 | While working Seq 2014, found J59 backshell not installed. | Avionics Tech | 2.5 |
| 17070 | While working Seq 2014, found harness clamps not secured inboard and aft of left hand hydraulic disconnect. | Avionics Tech | 1 |
| 17071 | While working Seq 2014, found harness not clamped through bulkhead inboard of left hand door post. | Avionics Tech | 2 |
| 17072 | While working Seq 2014, found hobbs switch has incorrect ground stud. | Avionics Tech | 1.25 |
| 17073 | While working Seq 2014, found harness clamp through floor below co-pilot collective control head hardware not tight. | Avionics Tech | 0.75 |
| 17074 | While working Seq 2014, found PRC lower antenna cracked. | Avionics Tech | 1.5 |
| 17078 | While working Seq 2014, found seal pins not installed on co-pilot cyclic J side connector. | Avionics Tech | 0.75 |
| 17079 | While working Seq 2014, found 2 ground studs left of terminal board 39 to have A5 corrosion and incorrect stack up. | Avionics Tech | 1 |
| 17082 | While working Seq 2014, found K27 mount and terminal hardware have A5 corrosion. | Avionics Tech | 1.5 |
| 17083 | While working Seq 2014, found 4 ground studs right of terminal board 39 to have A5 corrosion on hardware. | Avionics Tech | 1.25 |
| 17084 | While working Seq 2014, found 7 ground studs right of terminal board 39 to have A5 corrosion on hardware. | Avionics Tech | 1.5 |
| 17085 | While working Seq 2014, found terminal board 36 mount hardware and terminal post hardware to have A5 corrosion. | Avionics Tech | 2 |
| 17086 | While working Seq 2014, found terminal board 28 mount hardware and terminal post hardware have A5 corrosion. | Avionics Tech | 2 |
| 17088 | While working Seq 2014, found BFT circuit breaker amp placard missing. | Avionics Tech | 1.75 |
| 17089 | While working Seq 2014, found PRCE 152 wiring not cap and stowed. | Avionics Tech | 1.25 |
| 17094 | While working Seq 2014, found PRC hand held mount not secure. | Avionics Tech | 0.5 |
| 17096 | While working Seq 2014, found mag compass light inoperable. | Avionics Tech | 1.75 |
| 17099 | While working Seq 2014, found ALE harness not secured on glareshield. | Avionics Tech | 1 |
| 17102 | While working Seq 2014, found pilot ICS control faceplate has bleed through. | Avionics Tech (AVI) | 1 |
| 17103 | While working Seq 2014, found co-pilot ics control faceplate has bleed through. | Avionics Tech (AVI) | 1 |
| 17104 | While working Seq 2014, found fire handle control faceplate has bleed through. | Avionics Tech (AVI) | 1 |
| 17105 | While working Seq 2014, found right hand co-pilot airspeed light inoperable. | Avionics Tech (AVI) | 0.5 |
| 17106 | While working Seq 2014, found ENG control faceplate has bleed through. | Avionics Tech (AVI) | 1 |
| 17107 | While working Seq 2014, found hydraulic control faceplate has bleed through. | Avionics Tech (AVI) | 1 |
| 17108 | While working Seq 2014, found pilot collective faceplate has bleed through. | Avionics Tech (AVI) | 1 |
| 17109 | While working Seq 2014, found Lynx GPS antenna has screws not sealed. | Avionics Tech | 0.75 |
| 17110 | While working Seq 2014, found antenna aft of egg beater antenna screws not sealed. | Avionics Tech | 0.75 |
| 17111 | While working Seq 2014, found left hand position light hardware has A5 corrosion. | Avionics Tech | 1 |
| 17112 | While working Seq 2014, found ADF antenna has voids in proseal. | Avionics Tech | 1 |
| 17116 | While working Seq 2014, found ground stud at fuel capacitor has A5 corrosion. | Avionics Tech | 1 |
| 17118 | While working Seq 2014, found 12ea clamps from J96 down and around aft hellhole opening deteriorated. | Avionics Tech | 5 |
| 17119 | While working Seq 2014, found J168, P/N: MS3120E12-10S oil soaked and deteriorated. | Avionics Tech | 1.25 |
| 17120 | While working Seq 2014, found ground stud at forward end of right hand fuel cell to have A5 corrosion. | Avionics Tech | 1 |
| 17121 | While working Seq 2014, found 10ea clamps from J47 around to lighting hole into landing light deteriorated. | Avionics Tech | 5 |
| 17122 | While working Seq 2014, found #2 inverter mount hardware to have A5 corrosion. | Avionics Tech | 1.25 |
| 17123 | While working Seq 2014, found TB804 terminal hardware to have A5 corrosion. | Avionics Tech | 1 |
| 17124 | While working Seq 2014, found CR807 mount hardware to have A5 corrosion. | Avionics Tech | 1 |
| 17125 | While working Seq 2014, found connector and cap on J3816 corroded and rubber deteriorated. | Avionics Tech | 1.5 |
| 17126 | While working Seq 2014, found clamp forward and below NAV flash does not secure coax. | Avionics Tech | 1 |
| 17127 | While working Seq 2014, found clamp on harness at tailboom disconnect deteriorated. | Avionics Tech | 1 |
| 17128 | While working Seq 2014, found connector P169 seal pins not installed. | Avionics Tech | 0.75 |
| 17129 | While working Seq 2014, found 9ea clamps on harness from P169, 1678 and 187 deteriorated. | Avionics Tech | 3 |
| 17130 | While working Seq 2014, found 6 AAR/ALE connectors in right hand lower bay not capped properly. | Avionics Tech | 1 |
| 17131 | While working Seq 2014, found #1 inverter mount hardware has A5 corrosion. | Avionics Tech | 1.25 |
| 17132 | While working Seq 2014, found J60 backshell, P/N: M85049/52-1-28W not installed. | Avionics Tech | 2.5 |
| 17133 | While working Seq 2014, found harness and coax not secured forward of left hand fuel cell. | Avionics Tech | 1 |
| 17135 | While working Seq 2014, found right hand dome light lens cracked. | Avionics Tech | 1 |
| 17136 | While working Seq 2014, found ELT cap screws with A5 corrosion. | Avionics Tech | 0.75 |
| 17138 | While working Seq 2014, found search light terminal board cover screw not installed. | Avionics Tech | 0.75 |
| 17140 | While working Seq 2014, found forward left hand electrical bay has clamp at lower shelf left hand forward deteriorated. | Avionics Tech | 0.75 |
| 17141 | While working Seq 2014, found #1 inverter harness clamp loose. | Avionics Tech | 0.75 |
| 17144 | While working Seq 2014, found clamp right hand and aft of #2 inverter requires replacement. | Avionics Tech | 0.75 |
| 17145 | While working Seq 2014, found 5ea clamps on left hand aft ICS harness by air duct loose. | Avionics Tech | 2 |
| 17147 | While working Seq 2014, found #2 inverter safety loose. | Avionics Tech | 0.5 |
| 17149 | While working Seq 2014, found left hand FM coax not capped. | Avionics Tech | 0.5 |
| 17150 | While working Seq 2014, found left hand bracket hardware short on left hand side of forward left hand crew ICS control. | Avionics Tech | 0.75 |
| 17151 | While working Seq 2014, found IVHMMS harness not in clamp aft of left hand crew ICS control. | Avionics Tech | 0.75 |
| 17153 | While working Seq 2014, found 5ea clamps on right hand aft ICS harness by airduct loose. | Avionics Tech | 2 |
| 17154 | While working Seq 2014, found ELT cap screws with A5 corrosion. | Avionics Tech | 1.5 |
| 17155 | While working Seq 2014, found crew ICS controls missing TDFM decal. | Avionics Tech | 0.5 |
File details come from the government source that posted it. Updated .