UH-60 Repair Sample TO Discrepancy Report (RFP Attch X) DRAFT.xlsx
XLSX spreadsheet 23 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 statement of work outlines Programmed Depot Maintenance requirements for the Department of State's fleet of UH-1 aircraft, as well as potential H-60 repairs. The statement of work seeks a contractor to perform recurring Aircraft Condition Inspections, modifications, corrosion treatment and repair, component overhaul, and airframe refurbishment for UH-1 aircraft located in Peru, Iraq, Uruguay, Panama, Costa Rica, and the United States. The PDM program is expected to induct three Peruvian aircraft, two Iraqi aircraft, one Uruguayan aircraft, two Panamanian aircraft, and one Costa Rican aircraft per year. Additional U.S.-based aircraft are specified for fiscal years 2023, 2025, and 2026. Given the geographic distribution of aircraft, the Department of State is interested in the feasibility of conducting PDMs at a facility in Central or South America. Industry comments on the draft statement of work are requested 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 | |
| UH-1 PDM Sample TO Discrepancy Report (RFP Attch X) DRAFT.xlsx | XLSX spreadsheet | |
| Section M DRAFT UH-1 (series) PDM_H-60 (series) Repair DRAFT.docx | DOCX document | |
| 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
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 |
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