Attachment 3 - UH-60 Repair Sample TO Discrepancy Report.xlsx
XLSX spreadsheet 24 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 document contains a discrepancy report and federal contract opportunity for UH-60 helicopter repairs and maintenance. The discrepancy report lists over 200 maintenance issues found across multiple aircraft, including damaged seals, worn components, and required inspections. The related federal contract opportunity is a solicitation from the Department of State seeking offers for Programmed Depot Maintenance of UH-1 helicopters and repairs of H-60 aircraft. Offerors must submit electronic proposals by November 15, 2022. The solicitation involves maintenance and repair services for the State Department's rotary wing aircraft fleet.
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Other files
| File | Type | Posted |
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| UH-1 PDM QA Set 5 11-02-22.xlsx | XLSX spreadsheet | |
| UH-1 PDM QA Set 4 10-25-22.xlsx | XLSX spreadsheet | |
| Attachment 5 - GFP Inventory AUG22.xlsx | XLSX spreadsheet | |
| Attachment 4 - UH-1 PDM_H-60 Repair Labor Categories Rates Table.xlsx | XLSX spreadsheet | |
| Attachment 6 - UH-1 PDM_H-60 Repair SOW.docx | DOCX document | |
| Attachment 2 - UH-1 PDM Sample TO Discrepancy Report.xlsx | XLSX spreadsheet | |
| 19AQMM22R0006.pdf | ||
| Attachment 1 - Section B Fixed Price CLINs.xlsx | XLSX spreadsheet |
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Text version
484 Discrep
UH-60
OVER & ABOVE DISCREPANCIES BELOW
| Work Required | Corrective Action | Tech Labor Category | Tech Level (I, II, III) | # of Personnel | Base Labor Rate | Man Hours | Burdened Rate | Total | |
| CRITICAL | |||||||||
| Tail rotor gearbox cover rubber seal split. | Mech (Shop) | ||||||||
| Corrosion on right hand mount bushing to stab actuator. | Mech (Shop) | ||||||||
| Sludge build up noticed to inside of housing to tail rotor gearbox when removing tail rotor servo. | Mech (Shop) | ||||||||
| While performing Inspections on SEC 1, found right hand crew chief window forward and aft airframe seals delaminated. | Mech (Shop) | ||||||||
| While performing SEC 2 inspections, found 1ea right hand upper crew chief window brush seal not installed. | Mech (Shop) | ||||||||
| While performing inspections on SEC 1, found left hand crew chief window forward and aft airframe seals not installed. | Mech (Shop) | ||||||||
| While performing SEC 2 inspections, found cabin drip pan seal not installed. | Mech (Shop) | ||||||||
| Fuel system integrity test required. | Aircraft Mech | ||||||||
| While performing SEC 2 inspections, found 1ea right hand lower crew chief window crush real damaged. | Mech (Shop) | ||||||||
| While performing inspections on Seq 1, found right hand crew chief window forward and aft airframe seals delaminated. | Mech (Shop) | ||||||||
| While performing inspections on Seq 1, found left hand crew chief window forward and aft airframe seals not installed. | Mech (Shop) | ||||||||
| Tail rotor cable conduit to pylon at Hysol disbonded at multiple points. | Mech (Shop) | ||||||||
| Seq created for fire bottle stray voltage/operational check after installation. | Avionics Tech | ||||||||
| While working Seq 2002, found both pilot's and co-pilot's seats have multiple tears and delamination. | Mech (Shop) | ||||||||
| Aircraft requires 28VDC AUX port for USFS requirements. | Aircraft Mech | ||||||||
| ELT antenna mount requires fabrication. | Mech (Sheet Metal) | ||||||||
| Found wire W4404B24 degraded and broken when moved. | Avionics Tech | ||||||||
| While performing inspections on SEC 2, found small leak at APU accumulator hand pump. | Mech (Shop) | ||||||||
| While performing inspections on SEC 2, found left hand and right hand cargo door forward mating surface to airframe seals not installed. | Mech (Shop) | ||||||||
| During SEC 2 inspection Seq 2003, found the left hand and right hand upper cargo door seal to be torn and requires replacement. | Mech (Shop) | ||||||||
| During SEC 2 inspection on Seq 2003, found the left hand and the right hand aft airframe cargo door seal to be torn and requires replacement. | Mech (Shop) | ||||||||
| While performing inspection on SEC 2, found cabin steps over MLG shock struts gouged. | Mech (Sheet Metal) | ||||||||
| Seq created for removal of slime and IR lights from covers and repair. | Avionics Tech | ||||||||
| Seq created for removal of slime and IR lights from Stabilator and fabricate blank off plates. | Avionics Tech | ||||||||
| Heating and ventilation system heater duct outer seal has worn. | Mech (Shop) | ||||||||
| While working Seq 2003, found 8ea drag beam pivot bushings require replacement. | Mech (Shop) | ||||||||
| 2ea mounting bolts on right-center base plate pilot assist module manifold out of limits. | Aircraft Mech | ||||||||
| Main rotor hub has 19ea threaded inserts that have delamination beyond limits. | Mech (Shop) | ||||||||
| Tip cap to tail rotor, S/N: A398-17886 gouged, exceeds limits. | Mech (Sheet Metal) | ||||||||
| During PMI Inspections, found 1ea primary nozzle on APU to be bad. | Aircraft Mech | ||||||||
| Bushing to tail rotor pitch control shaft gouged beyond limits.. | Mech (Shop) | ||||||||
| During PMI Inspection, found tail lock pin broken. | Aircraft Mech | ||||||||
| NDI inspection (UT) required on tail rotor bevel gear, P/N: 70358-06620-102, S/N: G32002314. | Mech (Shop) | ||||||||
| During phase inspection, found left hand lower gunner window door track was found to be worn beyond limits and requires replacement. | Aircraft Mech | ||||||||
| During phase inspection, found center cabin floor has multiple areas of delamination requiring repair. | Mech (Sheet Metal) | ||||||||
| During PMI Inspection, found left hand pitot static line cracked under seat. | Avionics Tech | ||||||||
| While working Seq 2003, found cargo hook frame bushing teflon liner worn beyond limits. | Mech (Shop) | ||||||||
| Air inlet N*1 and N*2 lower fairing seal has broken. | Mech (Shop) | ||||||||
| Base plate pilot assist module 01 nut plate has worn beyond limits. | Mech (Shop) | ||||||||
| Seq created to perform main rotor, tail rotor, #1 engine and #2 engine rigging. | Aircraft Mech | ||||||||
| Sequence created to bleed and service brake system due to replacement of brake line. | Aircraft Mech | ||||||||
| Co-pilot's caster caution potentiometer has damaged legs. | Aircraft Mech | ||||||||
| Found #1 engine cowling latch bracket cracked. | Mech (Sheet Metal) | ||||||||
| Found 6ea working Hi-Lok fasteners on upper cabin area. | Mech (Sheet Metal) | ||||||||
| Cracked bracket at top of left hand firewall under APU inlet screen. | Mech (Sheet Metal) | ||||||||
| Cracked bracket at top of right hand firewall under APU inlet screen. | Mech (Sheet Metal) | ||||||||
| During main rotor flight control rigging, found collective balance spring tie bar hooks do not have .60 in exposed. | Aircraft Mech | ||||||||
| ELT battery is nonfunctional, requiring replacement. | Avionics Tech | ||||||||
| During modification, found cracked pitot static line in left hand pitot seat well, P/N: 70450-01059-062. | Avionics Tech | ||||||||
| During modification, found cracked pitot static line in right hand pilot seat well, P/N: 70450-01059-061. | Avionics Tech | ||||||||
| While working Seq 2007, found inner and outer bearing play beyond limits on all 4 main rotor dampers. | Mech (Shop) | ||||||||
| While performing inspections of Sec 1, left hand bulkhead brake line behind co-pilot's seat next to broom closet is gouged beyond acceptable limits. | Aircraft Mech | ||||||||
| During 48MO flight control rod inspection, found collective control rod end, P/N: 70400-02249-045, threads to be damaged beyond limits. | Mech (Shop) | ||||||||
| While working Seq 2109 48MO flight control rod inspection, found tail rotor spring cylinder terminal worn beyond limits IAW TM 1-1520-237-23-9 WP 1046. | Aircraft Mech | ||||||||
| While performing inspections on Seq 1, found right hand crew chief lower door track worn beyond limits. | Mech (Sheet Metal) | ||||||||
| MAJOR Discrepancy | |||||||||
| While performing Seq 1 inspections, found 1ea pin rivet damaged on pilot's side cockpit door lever bracket. | Mech (Sheet Metal) | ||||||||
| 7ea Total clamps to hydraulic lines located on forward and aft of tail rotor pylon damaged. | Aircraft Mech | ||||||||
| Hardware to incandescent position light to tail rotor gearbox cover worn at receptacle. | Avionics Tech | ||||||||
| Intermediate gearbox cover teflon tape worn. | Mech (Shop) | ||||||||
| While performing SEC V inspections, found chafe tape disbonded on forward tail rotor gearbox cover. | Mech (Shop) | ||||||||
| Pylon driveshaft cover teflon tape worn. | Mech (Shop) | ||||||||
| Seq created for replacement of tail landing gear tube and tire. Wheel bearing packing required. | Aircraft Mech | ||||||||
| Seq created for replacement of main landing gear tire and brake assembly, wheel bearing packing required. | Aircraft Mech | ||||||||
| While performing SEC 2 inspections, found 1ea nutplate not installed on cabin heating ventilation duct to hydraulic deck ducting. | Mech (Sheet Metal) | ||||||||
| While performing SEC 2 inspections, found wear marks on right hand lower cargo door track. | Mech (Sheet Metal) | ||||||||
| While working Seq 2002, found both pilot's and co-pilot's seats restraints missing required identification tags. | Mech (Shop) | ||||||||
| While performing inspections on Sec 1, found blank off plate on cockpit belly to be incorrectly shaped. | Mech (Sheet Metal) | ||||||||
| #2 collective mount cover velcro disbonded. | Mech (Shop) | ||||||||
| Seq created to replace main rotor spindle sleeve bearing, P/N: 70102-08200-069, S/N: A00112194. | Mech (Shop) | ||||||||
| Seq created to replace main rotor spindle sleeve bearing, P/N: 70102-08200-069, S/N: A00102250. | Mech (Shop) | ||||||||
| Seq created to replace main rotor spindle sleeve bearing, P/N: 70102-08200-069, S/N: A00112205. | Mech (Shop) | ||||||||
| Seq created to replace main rotor spindle sleeve bearing, P/N: 70102-08200-069, S/N: A00112193. | Mech (Shop) | ||||||||
| Engine #2 outer mount strut bearing has worn beyond limits. | Mech (Shop) | ||||||||
| Tip cap to tail rotor, S/N: A398-14827, gouged within limits. | Mech (Shop) | ||||||||
| While working Seq 2003, found right hand drag beam pivot bushings to be out of limits, requiring replacement. | Mech (Shop) | ||||||||
| Engine #1 inner mount strut bearing has worn beyond limits. | Mech (Shop) | ||||||||
| Engine air inlet 01 eccentric pin not installed. | Mech (Shop) | ||||||||
| Engine #1, 2ea inner mount links have worn beyond limits. | Mech (Shop) | ||||||||
| Engine #2, 2ea outer mount links have worn beyond limits. | Mech (Shop) | ||||||||
| While performing section 4 inspection, found tail wheel fork lock ring groove to be beyond limits. | Mech (Shop) | ||||||||
| During PMI Inspection, found left hand and right hand APU screen has multiple cracks. | Aircraft Mech | ||||||||
| Working Seq 2005, found tail wheel yoke teflon washers disbonded, IAW DE TM 1-1520-237-23-6. | Mech (Shop) | ||||||||
| During PMI Inspection, found lockpin bushing and fork wearplate out of limits. | Mech (Shop) | ||||||||
| While working Seq 2006, found tail rotor blade abrasion strip torn. | Mech (Shop) | ||||||||
| Main rotor red pitch control rod upper and lower rod end is damaged, requiring replacement. | Mech (Shop) | ||||||||
| Replace oil cooler radiator inlet line due to present leak on 45 degree elbow. | Aircraft Mech | ||||||||
| While working Seq 2005, found tail wheel lock pin and actuator deformed beyond limits, IAW DE TM 1-1520-237-23--6 WP 473. | Aircraft Mech | ||||||||
| Replace main rotor sliding cover track that have 3ea wear strips showing wear beyond limits. | Mech (Sheet Metal) | ||||||||
| NDI eddy current inspection required on drag beam supper fitting lugs, P/N: 70211-02501-011, and P/N: 70211-02504-012. | Mech (Shop) | ||||||||
| Seq created for servicing all landing gear shock struts. | Aircraft Mech | ||||||||
| While working Seq 2007, found both left hand and right hand engine bracket bearings worn beyond limits. | Mech (Shop) | ||||||||
| During phase inspection, found cargo hook door hinges were found to be cracked and require replacement. | Mech (Sheet Metal) | ||||||||
| While working Seq 2003, found left hand cargo door had a repairable dent on center of outside door skin. | Mech (Sheet Metal) | ||||||||
| While working Seq 2003, found right hand cargo door had a repairable dent on upper center of inside door skin. | Mech (Sheet Metal) | ||||||||
| Seq created to flush fill right hand step fairing position light hole to fit new LED position light. | Mech (Sheet Metal) | ||||||||
| Found multiple cabin heater ducting cracked at fitting ends. | Mech (Sheet Metal) | ||||||||
| Found right hand pilot cyclic boot torn in multiple places. | Aircraft Mech | ||||||||
| Sequence created for QC final inspection over aircraft and final record review post phase and build. | Aircraft Mech (QA) | ||||||||
| During PMI found wiper arm bracket broken. | Aircraft Mech | ||||||||
| AC requires power on testing. | Avionics Tech | ||||||||
| While unmasking main rotor head, found black main rotor damper indicator leaking . | Mech (Shop) | ||||||||
| While unmasking main rotor head, found blue main rotor damper indicator was painted on indicating surface. | Mech (Shop) | ||||||||
| Sequence created to fill modified right hand step fairing to original step fairing configuration. | Mech (Sheet Metal) | ||||||||
| ASN43 latitude knob missing degree markings. | Avionics Tech | ||||||||
| Comply with H-60-20-AMAM-03 for Pickering Type Certificate Compliance. | Aircraft Mech (QA) | ||||||||
| #1 fire bottle main discharged during stray voltage check. P/N: 05167-30400004-1, S/N: 27358 B1.) | Aircraft Mech | ||||||||
| NDI required on tail rotor outboard split cones, P/N: 70358-06343-103, S/N: D403-01595. | Mech (Shop) | ||||||||
| NDI required on tail rotor inboard split cones, P/N: 70358-06343-102, S/N: E402-08783. | Mech (Shop) | ||||||||
| NDI required on Tail rotor spring capsule support terminal bearing bores, P/N: 70400-06670-044. | Mech (Shop) | ||||||||
| NDI required on 4ea LDS/PAS housing assemblies, P/N: 70301-02115-101. | Mech (Shop) | ||||||||
| NDI required on 4ea LDS/PAS housing assemblies, P/N: 70301-02112-041. | Mech (Shop) | ||||||||
| NDI required on 4ea LDS/PAS housing assemblies, P/N: 70301-02113-041. | Mech (Shop) | ||||||||
| NDI required on main rotor spindle lugs, P/N: 70102-08200-069, S/N: A00102250. | Mech (Shop) | ||||||||
| NDI required on main rotor spindle lugs, P/N: 70102-08200-069, S/N: A00112194. | Mech (Shop) | ||||||||
| NDI required on main rotor spindle lugs, P/N: 70102-08200-069, S/N: A00112205. | Mech (Shop) | ||||||||
| NDI required on main rotor spindle lugs, P/N: 70102-08200-069, S/N: A00112193. | Mech (Shop) | ||||||||
| NDI required on tail rotor bevel gear, P/N: 70358-06620-102, S/N: C321000990. | Mech (Shop) | ||||||||
| NDI required on tail wheel halves assembly, P/N: 70250-13005-103, S/N: JUL15-10563. | Mech (Shop) | ||||||||
| NDI required on #2 engine bracket, P/N: 70305-02110-043. | Mech (Shop) | ||||||||
| NDI required on #2 engine strut, P/N: 70305-02106-044. | Mech (Shop) | ||||||||
| NDI required on #1 engine strut, P/N: 70305-002105-045. | Mech (Shop) | ||||||||
| NDI required on #1 engine bracket, P/N: 70305-02111-043. | Mech (Shop) | ||||||||
| NDI required on #1 engine fitting, P/N: 70305-02110-043. | Mech (Shop) | ||||||||
| While performing inspections on Seq 1, found right hand windshield delaminated. | Aircraft Mech | ||||||||
| During modification, found pedestal left hand tie down strap broken. | Mech (Sheet Metal) | ||||||||
| During repair of left hand cargo door upper track seal, found left hand lower engine drain duct fairing cracked. | Mech (Shop) | ||||||||
| Tail rotor pitch control rods, 3ea, upper rod end and 4ea lower rod end has crack beyond limits. | Mech (Shop) | ||||||||
| Comply with H-60-22-ASAM-06 Main generator chafing. | Avionics Tech | ||||||||
| Comply with H-60-20-ASAM-04 24-Month MRB Tap Test. | Aircraft Mech (QA) | ||||||||
| During PMD, found 1ea tail rotor abrasion strip came off during flight. | Mech (Shop) | ||||||||
| Aircraft requires ring out of avionics system. | Avionics Tech | ||||||||
| Sequence created to procure and install lower right hand instrument panel edge foam. | Avionics Tech | ||||||||
| A020 inspection, main rotor spindle lugs, main rotor cuff, tip cap inspection due per AC log book. | Aircraft Mech | ||||||||
| A092 Inspection, 30 day slab battery inspection, S/N: D8565.11.1, due per AC log book. | Aircraft Mech | ||||||||
| A0103 inspection, aircraft wash due per AC logbook. | Aircraft Mech | ||||||||
| A110 Inspection: 40HR inspection due per A/C logbook. | Aircraft Mech | ||||||||
| A115 Inspection: 30 day lube requirements due per A/C log book. | Aircraft Mech | ||||||||
| A116 Inspection: Intermediate gearbox oil sample due per A/C log book. | Aircraft Mech | ||||||||
| A117 Inspection: Tail gearbox oil sample due per A/C logbook. | Aircraft Mech | ||||||||
| A160 Inspection: 90 Day Corrosion inspection due per A/C logbook. | Aircraft Mech | ||||||||
| A177 Inspection: 90 day review/update of 365-4 entries due per A/C logbook. | Aircraft Mech (QA) | ||||||||
| A210 Inspection: 120 hour inspection due per A/C log book. | Aircraft Mech | ||||||||
| A211 Inspection: APU oil sample due per A/C logbook. | Aircraft Mech | ||||||||
| A213 Inspection: engine compressor cleaning due per A/C logbook. | Aircraft Mech | ||||||||
| A214 Inspection: Clean tail wheel adapter due per A/C logbook. | Aircraft Mech | ||||||||
| A230 Inspection: Battery compartment corrosion inspection due per A/C logbook. | Aircraft Mech | ||||||||
| A288 Inspection: Fuel nozzle assembly inspection (garrett/honeywell) due per A/C logbook. | Aircraft Mech | ||||||||
| A289 Inspection: Orifice fitting inspection, (garrett/honeywell) due per A/C logbook. | Aircraft Mech | ||||||||
| A290 Inspection: Igniter plug assembly inspection (garrett/honeywell) due per A/C logbook. | Aircraft Mech | ||||||||
| A291 Inspection: Magnetic drain plug assembly inspection (garrett/honeywell) due per A/C logbook. | Aircraft Mech | ||||||||
| A292 Inspection: Drain/refill lubricating oil (Garrett/Honeywell) due per A/C logbook. | Aircraft Mech | ||||||||
| A293 Inspection: Remove and replace oil filter element (garrett/honeywell) due per A/C logbook. | Aircraft Mech | ||||||||
| A301 Inspection: Torque inner and outer swashplate duplex bearing retainer ring bolts due per A/C logbook. | Aircraft Mech | ||||||||
| A302 Inspection: Lubricate main landing gear wheel bearings due per A/C logbook. | Aircraft Mech | ||||||||
| A303 Inspection: Inspect left hand and right hand relay panels due per A/C logbook. | Aircraft Mech | ||||||||
| A320 Inspection: Engine inspection cleaning due per A/C logbook. | Aircraft Mech | ||||||||
| A408 Inspection: 960 hour lube requirements (PMI-2 Area 5 and 6) per A/C log book. | Aircraft Mech | ||||||||
| A410 Inspection: 960 Hour lube requirements (PMI-1 area 1 through 4) due per A/C log book. | Aircraft Mech | ||||||||
| A415 Inspection: Main gearbox oil samples - P/N: 073, 374, 076 due per A/C log book. | Aircraft Mech | ||||||||
| A440 Inspection: Clean tail wheel lockpin due per A/C logbook. | Aircraft Mech | ||||||||
| A440 Inspection: CF2BR fire extinguisher weight test inspection due per A/C logbook. | Aircraft Mech | ||||||||
| A501 Inspection: main rotor blade spar pressure check due per A/C log book. | Aircraft Mech | ||||||||
| A502 Inspection: Inspect and test ground receptacle due per A/C log book. | Avionics Tech | ||||||||
| A5330 Inspection: aircraft equipment inventory (DA Form 2408-17) due per A/C logbook . | Aircraft Mech (QA) | ||||||||
| A532 Inspection: Compass swing/RMI due per A/C logbook. | Pilot | ||||||||
| A541 Inspection: Replace digital clock battery due per A/C Logbook. | Avionics Tech | ||||||||
| A538 Inspection: FAT-OAT gauge inspection test due per A/C logbook. | Aircraft Mech (QA) | ||||||||
| A533 inspection: pitot static system inspection due per A/C logbook. | Avionics Tech | ||||||||
| A534 Inspection: First aid kit inspection due per A/C logbook. | Mech (Shop) | ||||||||
| A580 Inspection: return slab battery to AVIM for capacity check (24MO) due per A/C logbook. | Mech (Shop) | ||||||||
| E220 Inspection: emergency locator transmitter self-test as required due per A/C logbook. | Avionics Tech | ||||||||
| E222 Inspection: emergency locator transmitter (ELT) registration update due per A/C logbook. | Avionics Tech | ||||||||
| E325 Inspection: replacement of ELT battery, P/N: GS-46 (EBC-406HM) due per A/C logbook. | Avionics Tech | ||||||||
| E331 Inspection underwater acoustic beacon test and clean due per A/C logbook. | Avionics Tech | ||||||||
| MINOR | |||||||||
| Sequence created to perform PMD as required. | |||||||||
| Seq created to replace 5ea door locks as matched sets. | Aircraft Mech | ||||||||
| Task created to capture labor associated with ballast box installation. | Aircraft Mech | ||||||||
| Sequence created to procure required operational placards for center console. | |||||||||
| Seq created to procure plugs and covers for A/C. | Supply Tech | ||||||||
| Seq created to send main rotor blade to vendor for evaluation, repair, and high visibility paint, P/N: 70150-09100-043, S/N: A007-02010. | |||||||||
| Seq created to send main rotor blade to vendor for evaluation, repair, and high visibility paint, P/N: 70150-09100-043, S/N: A007-12404. | |||||||||
| Seq created to send main rotor blade to vendor for evaluation, repair, and high visibility paint, P/N: 70150-09100-043, S/N: A007-04576. | |||||||||
| Task created for procurement of 2ea P/N: 133956-1, a filter, for use on sequence 1021. | Supply Tech | ||||||||
| Seq created for inspection of troop seats. | Aircraft Mech |
19AQMM22R0006 UH60 REPAIR SAMPLE TASK ORDER DISCREPANCY REPORT ATTACHMENT 3
&1#&"Times New Roman"&10&K000000SENSITIVE BUT UNCLASSIFIED
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