# Service difficulty reports: N762DA, cancelled Jun 4, 2010 A list on [N762DA, cancelled Jun 4, 2010](https://openairdocs.org/deregistered/N762DA-2010-06-04.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR DLL19982045](https://openairdocs.org/sdr/DLL19982045.md): Oil Syst · leaking · Oct 4, 1998 · N762DA · Lkheed 10113853 · APU Oil System > AFTER T/O, HAD ODOR AS DESCRIBED IN PREVIOUS WRITE UP THIS. DISSIPATED UNTIL DESCENT INITATED, THEN WHOLE CABIN AND FLT DECK FILLED WITH A VAPOR SMOKE. FOUND APU INTERNAL OIL LEAK. - [SDR DLL19982041](https://openairdocs.org/sdr/DLL19982041.md): Coalescer · contaminated · Oct 3, 1998 · N762DA · Lkheed 10113853 · Humidity Control System > OILY SMELL IN 1ST CLASS CABIN AND C/P SMELL SEEMED NEARLY DISAPPEARED WITH NR 2 PACK OFF. RAN ENGINES PER PFHB AND PACKS ISOLATED SMELL TO NR 1 PACK. REPLACED COALESCER. - [SDR DLL19981162](https://openairdocs.org/sdr/DLL19981162.md): Rear Spar · cracked · May 29, 1998 · N762DA · Lkheed 10113853 · Wing Spar > THE LT WING REAR SPAR WAS FOUND WITH TWO CRACKED FASTENER HOLES COMMON TO THE UPPER WING SKIN AND SPAR CAP AT APPROX IWS 322. THE CRACKS WERE FOUND DURING ROUTINE INSPECTIONS AND WERE REMOVED BY OVERSIZING THE HOLES. THE OVERSIZE HOLES WERE COLD WORKED, BU - [SDR DLL19981161](https://openairdocs.org/sdr/DLL19981161.md): Rear Spar · cracked · May 29, 1998 · N762DA · Lkheed 10113853 · Wing Spar > THE RT WING REAR SPAR WAS FOUND WITH TWO CRACKED FASTENER HOLES DURING ROUTINE INSPECTIONS. ONE HOLE WAS COMMON TO THE UPPER WING SKIN AND SPAR CAP AND THE OTHER TO THE SPAR WEB AND UPPER CAP. BOTH HOLES WERE APPROX AT IWS 322. BOTH HOLES WERE OVERSIZED T - [SDR DLL19980844](https://openairdocs.org/sdr/DLL19980844.md): Tr Light · illuminated · Apr 19, 1998 · N762DA · Lkheed 10113853 · Engine Thrust Reverser > REVERSER PRESSURE LIGHT ON IN FLT POM. FOUND REVERSER STOWED AND REPLACED PRSOV WITH NO HELP. SUSPECT WIRING. - [SDR DLL19972198](https://openairdocs.org/sdr/DLL19972198.md): Bulkhead Web · corroded · Oct 17, 1997 · N762DA · Lkheed 10113853 · Fuselage Main, Bulkhead > FUSELAGE BULKHEAD FS 328 LBL 15 WL 127 REPAIR FOR CORROSION CUT OUT IN WEB. THE FS 328 NLG WHEEL WELL PRESSURE BULKHEAD WAS FOUND CORRODED AT WL 127, LBL 15. THE CORROSION REMOVAL RESULTED IN A 2.8 BY 1.6 RECTANGULAR CUT OUT IN THE WEB. A DOUBLER REPAIR WAS - [SDR DLL19972196](https://openairdocs.org/sdr/DLL19972196.md): Longeron · corroded · Oct 17, 1997 · N762DA · Lkheed 10113853 · Fuselage Main, Longeron/Stringer > FUSELAGE NOSE LG WHEEL WELL LWR LONGERON LBL 22, FS353 REPAIR FOR CORROSION DAMAGE. THE NLG WHEEL WELL LONGERON AT LBL 22, FS 353 WAS FOUND WITH EXTENSIVE CORROSION REQUIRED A SECTION TO BE CUT OUT. A NEW SECTION WAS SPLICED IN PER ER/A 362972-14. - [SDR DLL16971754](https://openairdocs.org/sdr/DLL16971754.md): Gearbox · failed · Sep 8, 1997 · N762DA · Lkheed 10113853 · Turbine Engine Accessory Drive > NR 3 ENG FLAME-OUT, NO OIL PRESS/NO N3/N1, N2 WINDMILLING NORMAL. OIL QUANTITY 19 QTS OCCURED IN CRZ AT FL 330. REPLACED GEARBOX. - [SDR DLL16971255](https://openairdocs.org/sdr/DLL16971255.md): Power Supply · inoperative · Jun 27, 1997 · N762DA · Lkheed 10113853 · Emergency Lighting > RIGHT HAND AFT SIDE EMERGENCY TRACK LIGHTS DID NOT ILLUMINATE DURING TEST. REPLACED POWER SUPPLY, OP CKS GOOD. - [SDR DLL16971232](https://openairdocs.org/sdr/DLL16971232.md): Power Supply · inop · Jun 24, 1997 · N762DA · Lkheed 10113853 · Emergency Lighting > FWD RT OVHD EMERGENCY LIGHT WOULD NOT TEST. REPLACED POWER SUPPLY, CHECKS NORMAL. - [SDR DLL16970193](https://openairdocs.org/sdr/DLL16970193.md): Regulator Valve · sheared · Jan 31, 1997 · N762DA · Lkheed 10113853 · Landing Gear Retraction/Extension System > SHIP 762 DIVERTED NCE/LGW DUE TO C-SYSTEM HYDRAULIC LOSS AFTER GEAR SELECTED UP. ON ARRIVAL LGW, FOUND FLOW REGULATOR VALVE SHEARED P/N AV20A1032-107 ON LANDING GEAR CONTROL MODULE P/N 1505607-135. REPLACED FLOW REGULATOR VALVE PER M.M. AND PERFORMED - [SDR DLL16970053](https://openairdocs.org/sdr/DLL16970053.md): Fuel Manifold · cracked · Jan 12, 1997 · N762DA · Lkheed 10113853 · Engine Fuel Distribution > SHUTDOWN NR 3 ENG ON FINAL/DESCENT. LOW OIL PRESS LIGHT CAME ON AND OIL PRESS DROPPED BELOW 18 PSI LONGER THAN 45 SEC. OIL PRESS WAS PRECEDED BY THE LOSS OF THROTTLE, RESPONSE FOR NR 3 ENG. FOUND FUEL MANIFOLD LINE AT NR 14 FUEL NOZZLE BROKEN. REPLACED FU - [SDR DLL16962604](https://openairdocs.org/sdr/DLL16962604.md): Throttle Lever · stuck · Nov 28, 1996 · N762DA · Lkheed 10113853 · Power Lever > NR 3 THROTTLE WILL NOT RETARD PAST 2.2 UNITS ON DESCENT. ALSO, STIFF TO MOVE FWD BUT WILL MOVE FWD, HAD TO SHUT DOWN NR 3 ENG. NIL FAULT OR WEAR FOUND THROTTLE MOVEMENT CHECKED THROUGH COMPLETE RANGE AND FOUND NORMAL WITH NO EXCESSIVE FORCE REQUIRED. BASIC - [SDR DLL16962267](https://openairdocs.org/sdr/DLL16962267.md): Skin · cracked · Oct 3, 1996 · N762DA · Lkheed 10113853 · Wing, Plate/Skin > A CRACK WAS FOUND IN THE UPPER WING SKIN AT THE REAR SPAR UPPER CAP ATTACH LOCATION IN THE FWD ROW AT APPROX IWS 324 AND IN THE AFT ROW AT IWS 329. THE CRACKS WERE REMOVED BY OVERSIZING NEARBY HOLES. - [SDR DLL16954272](https://openairdocs.org/sdr/DLL16954272.md): Switch · inop · Nov 7, 1995 · N762DA · Lkheed 10113853 · Fuel Controlling System > ATL - ON CLIMBOUT, NR 2 ENG WOULD NOT DEVELOPE CLIMB POWER. REPLACED ALTITUDE PRESS SWITCH. - [SDR DLL16954502](https://openairdocs.org/sdr/DLL16954502.md): Blkhd Cap · cracked · Nov 4, 1995 · N762DA · Lkheed 10113853 · Fuselage Main, Bulkhead > THE STA 449 BULKHEAD CAP WAS FOUND WITH A 7 INCH LONG CRACK IN ITS BEND RADIUS AT RBL 90.70. REPAIRED PER DL ERA 272084-14. - [SDR DLL16954314](https://openairdocs.org/sdr/DLL16954314.md): Rear Spar · cracked · Nov 2, 1995 · N762DA · Lkheed 10113853 · Wing Spar > DURING THE ACCOMPLISHMENT OF EO 7-59089-3 FOR THE RIGHT WING, CRACKS WERE FOUND EMANATING FROM EXISTING FASTENERS HOLES BETWEEN IWS 293.58 AND IWS 346.109. THE CRACKS WERE FOUND IN THE REAR SPAR UPPER CAP AT LOCATION 12A AND IN THE REAR SPAR WEB AT LOCATION 1 - [SDR DLL16954313](https://openairdocs.org/sdr/DLL16954313.md): Latch Fittings · corrosion · Nov 2, 1995 · N762DA · Lkheed 10113853 · Cargo/Baggage Doors > DURING THE ACCOMPLISHMENT OF SI 7-58181-12AD, THE NR 1, 2, 3 AND 8 C-1A CARGO DOOR LATCH FITTINGS WERE FOUND WITH SURFACE CORROSION IN THE UPPER WELL. ALSO, DRAIN HOLES IN THE CENTER OF THE LOWER WEB WERE ADDED FOR ALL 8 OF THE SUBJECT FITTINGS. THE SURFACE - [SDR DLL16954311](https://openairdocs.org/sdr/DLL16954311.md): Blkhd Frame · corroded · Oct 30, 1995 · N762DA · Lkheed 10113853 · Fuselage Main, Bulkhead > THE AFT P-DOME FRAME SEGMENTS BETWEEN S-22 AND S-44 WERE FOUND WITH CRACKS IN THE LOWER FLANGE RADIUS. THE FRAME SEGMENTS ARE MADE FROM.050 THICK 7178-T6 AL SHEET. ALSO, THE FRAME WEB BETWEEN S-44 AND S-33 WAS FOUND BADLY CORRODED. THE WEB IS FABRICATED FR - [SDR DLL16954310](https://openairdocs.org/sdr/DLL16954310.md): Skin · oversized holes · Oct 30, 1995 · N762DA · Lkheed 10113853 · Wing, Plate/Skin > WHILE ACCOMPLISHING OPN104 OF EO 7-57989-3, FASTENER HOLES 1 A AND B THROUGH 8 A AND B, 16 HOLES IN BAY 12 WERE FOUND TO HAVE OVERSIZED FASTENERS. ALREADY INSTALLED THROUGH THE REAR SPAR LOWER CAP AND LOWER WING SKIN. REPAIR APPROVAL PER DL ERA 272150-14. - [SDR DLL16954533](https://openairdocs.org/sdr/DLL16954533.md): Skin · corroded · Oct 19, 1995 · N762DA · Lkheed 10113853 · Fuselage Main, Plate/Skin > THE FUSELAGE SKIN PANEL WAS CUT TO REMOVE CORROSION FROM STA 1423 TO 1453 AT STR 35. REPAIRED PER DL ERA 272098-14. - [SDR DLL16954505](https://openairdocs.org/sdr/DLL16954505.md): Skin · corroded · Oct 19, 1995 · N762DA · Lkheed 10113853 · Fuselage Main, Plate/Skin > THE FUSELAGE SKIN BET FS 1545, FS 1565 AND AT STR 36 WAS CORRODED AND GROUND BEYOND LIMITS. REPAIRED PER DL ERA 272061-14. - [SDR DLL16954312](https://openairdocs.org/sdr/DLL16954312.md): Skin · corrosion · Oct 13, 1995 · N762DA · Lkheed 10113853 · Fuselage Main, Plate/Skin > DURING CORROSION REMOVAL, AN AREA OF SKIN AND TWO LAYERS OF BONDED SKIN WERE TRIMMED OUT IN A 9.5 INCH BY 8.75 INCH CUT OUT AT STA 1625 STRINGER 30. ALSO, THE AFT EDGE OF THE DOOR TRIPLER WAS NOTCHED APPROXIMATELY 6 INCHES IN LENGTH AND.75 INCH INTO THE STRA - [SDR DLL16954152](https://openairdocs.org/sdr/DLL16954152.md): Floor Beam · corroded · Oct 7, 1995 · N762DA · Lkheed 10113853 · Fuselage Main, Floor Beam > AT HMV, FOUND CABIN FLOOR BEAM CORRODED AT FS 1763 AT RBL 442, 76, 81, 86 AND 91. REPLACED FLOOR BEAM CAP PER SRM 53-21-00, PG 849-852. - [SDR DLL16954151](https://openairdocs.org/sdr/DLL16954151.md): Seat Track · corroded · Oct 7, 1995 · N762DA · Lkheed 10113853 · Fuselage, Seat/Cargo Attach Fittings > AT HMV, FOUND LBL 30 SEAT TRACK CORRODED AT FS 1665 TO FS 1725. REPAIRED PER SRM 53-21-00 PG 836-840. - [SDR DLL16954008](https://openairdocs.org/sdr/DLL16954008.md): Floorbeam · corroded · Oct 7, 1995 · N762DA · Lkheed 10113853 · Fuselage Main, Floor Beam > THE FS 886 FLOORBEAM WAS CORRODED ON THE UPPER CAP AT APPROX RBL 30. THE DAMAGE WAS OUT OF LIMITS SO THE REPAIR WAS ACCOMPLISHED PER SRM 53-21-00 PAGES 823 TO 824. - [SDR DLL16954007](https://openairdocs.org/sdr/DLL16954007.md): Floorbeam · corroded · Oct 7, 1995 · N762DA · Lkheed 10113853 · Fuselage Main, Floor Beam > THE FS 901 BEAM WAS CORRODED AT LBL 45. THE DAMAGE WAS FOUND TO BE OUT OF LIMITS PER SRM 53-21-00 PAGES 849 TO 852. - [SDR DLL16953204](https://openairdocs.org/sdr/DLL16953204.md): Line · failed · Jul 27, 1995 · N762DA · Lkheed 10113853 · Hydraulic System, Main > A/C DIVERTED INTO JFK WITH C-HYD SYSTEM FAILURE. FOUND LEAKING PRESSURE LINE NR 2 ENG HYD PRESS FILTER IPC, REF 29-11-53 FIG 1 PG 0 ITEM NR 95. INSTALLED NEW LINE AND AS PRECAUTION REPLACED PUMP AND FILTER, OPERATION NORMAL. - [SDR DLL16952120](https://openairdocs.org/sdr/DLL16952120.md): Oil Cap · leaking · May 12, 1995 · N762DA · Lkheed 10113853 · Turbine Engine Oil System > DURING CRUISE HAD EXCESSIVE OIL LOSS ON NR 2 ENGINE, 6 QTS IN IN ABOUT 3 HOURS, LANDED LGW. FOUND OIL TANK OIL CAP LEAKING THROUGH LOCK ASSEMBLY. REPLACED OIL CAP RETURNED TO SERVICE. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N762DA' AND deregistration_id = 'N762DA-2010-06-04' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N762DA-2010-06-04/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.