N938AS, cancelled Mar 21, 2013

Service difficulty reports · 54

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N938AS' AND deregistration_id = 'N938AS-2013-03-21'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR CALA0001204Actuator · burnedBOTH CREW MEMBERS NOTICED A STRONG ELECTRICAL ODOR IN THE COCKPIT DURING CLIMB OUT OF TPA. CREW WAS UNABLE TO ISOLATE THE SOURCE AND THE AIRCRAFT WAS RETURNED TO TPA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AUTO SPOILER ACTUATOR IN FORWARD PEDAug 3, 2000 · N938AS · Doug DC982 · Drag Control ActuatorSDR CALA0000400Frame · wornINSPECTION FOUND A HOLE WORN THROUGH FRAME WEB AT STA 1380, LONGERON 4L. THE FRAME WAS REPAIRED IAW SRM 53-01, FIGURE 4.Apr 4, 2000 · N938AS · Doug DC982 · Fuselage Main, FrameSDR CALA0000378Pan · corrodedINSPECTION FOUND E&E DOOR PAN CORRODED BETWEEN THE PAN AND THE E&E DOOR SWITCH AT STA 143, RBL 28. THE CORROSION WAS REMOVED IAW SRM 51-10-03. THE SWITCH BRACKET AND FITTINGS WERE REMOVED IAW SRM 51-30-01 AND 51-30-05. A REPAIR DOUBLER WAS INSTALLED IAW SRMMar 31, 2000 · N938AS · Doug DC982 · Electrical/Electronic Compartment DoorsSDR CALA0000377Seat Track · gougedINSPECTION FOUND LEFT O/B CABIN SEAT TRACK GOUGED AT STA 1245, LBL 54.5. THE SEAT TRACK SECTION WAS REMOVED AND REPLACED IAW SRM 51-10-03.Mar 31, 2000 · N938AS · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000372Angle · corrodedINSPECTION FOUND AFT PRESSURE BULKHEAD SIDE LOWER JACK PAD SUPPORT ANGLE CORRODED AT STA 1138, LONGERON 29R. THE JACK PAD HAT ANGLE JACK SUPPORT, STIFFENERS, AND LONGERON FITTINGS WERE REMOVED AND NEW PARTS WERE INSTALLED IAW SRM 51-30-05, 51-30-02.Mar 30, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000363Pan · crackedINSPECTION FOUND AFT CARGO DOOR FORWARD END INNER PAN CRACKED BY CARGO DOOR LATCHES. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-04, 51-30-05, 51-10-03, AND 52-05, FIGURE 26A.Mar 28, 2000 · N938AS · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000362Web · corrodedINSPECTION FOUND LT O/B CUSP WEB CORRODED AT FS 1250, LBL 60. THE CORRODED AREAS WERE REMOVED IAW SRM 53-01, FIGURE 4. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-01, FIGURE 4 AND 53-10-03.Mar 28, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000361Strap · crackedINSPECTION FOUND A 1.3 INCH CRACK IN LOWER FORWARD CORNER L-1 DOOR TIE STRAP. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-30-02.Mar 28, 2000 · N938AS · Doug DC982 · Passenger/Crew DoorsSDR CALA0000360Pan · corrodedINSPECTION FOUND E & E DOOR PAN CORRODED AROUND AND BETWEEN FWD AND AFT DOOR LOCK FITTINGS AT STA 138 & 148, RBL 28. THE DOOR PAN WAS REPAIRED IAW ECRA 5310-03995.Mar 28, 2000 · N938AS · Doug DC982 · Passenger/Crew DoorsSDR CALA0000359Fitting · crackedINSPECTION FOUND A 2 INCH CRACK IN FLOOR FITTING AND INTERCOSTAL CORRODED IN FORWARD PIT AT STA 427, L29R. THE FITTING AND INTERCOSTAL WERE REMOVED IAW SRM 51-30-01 AND 51-20-01. A NEW INTERCOSTAL AND FITTING WERE INSTALLED IAW SRM 51-30-02, 51-10-03, AND 51Mar 28, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000358Strap · corrodedINSPECTION FOUND AFT CARGO DOOR LOWER JAMB REPAIR STRAP CORRODED AT FS 1193 - 1212, LONGERON 27R. THE REPAIR STRAP WAS REMOVED AND REPLACED IAW SRM 51-10-4, 51-30-05, AND ECRA 5310-03027.Mar 28, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000357Fitting · corrodedINSPECTION FOUND FLOOR FITTING JUST I/B OF AFT CORNER OF R-1 DOOR, FS 208, RBL 48 CORRODED. THE FLOOR FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-01, 51-10-03, 51-10-04, AND 51-30-02.Mar 28, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000341Angle · crackedINSPECTION FOUND LEFT AFT EMERGENCY EXIT DOOR LOWER AFT CORNER SUPPORT ANGLE CRACKED AROUND FASTENER HOLES AND SURFACE CORROSION WAS PRESENT. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-10 AND 51-70-04.Mar 24, 2000 · N938AS · Doug DC982 · Emergency ExitsSDR CALA0000338Web · crackedINSPECTION FOUND A 3 INCH CRACK AT FASTENER HOLE OF LT O/B CUSP WEB NEAR SEAT TRACK SPLICE FOR LT O/B SEAT TRACK, FS 1220. THE CRACKED AREA OF CUSP WEB WAS REMOVED IAW SRM 53-01. DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-01, 51-10-03, AND 53-01-04.Mar 23, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000337Skin · dentedINSPECTION FOUND AFT CARGO DOOR SKIN DENTED. THE DOOR SKIN WAS REPAIRED IAW SRM 53-04, FIGURE 38 AND 51-30-01.Mar 23, 2000 · N938AS · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000336Support Bracket · crackedINSPECTION FOUND EXTERNAL FUSELAGE SUPPORT BRACKET CRACKED AT STA 798, LONGERON 20R. THE BRACKET WAS REMOVED AND REPAIR WAS INSTALLED IAW SRM 51-30-01, 51-10-04, 51-10-03, AND 51-30-05.Mar 23, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000335Seat Track · corrodedINSPECTION FOUND LEFT I/B CABIN SEAT TRACK CORRODED FROM STA 1155 - 1212. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK AND SPLICE WERE INSTALLED IAW SRM 51-30-05 AND 51-30-01.Mar 23, 2000 · N938AS · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000334Pan · crackedINSPECTION FOUND AFT CARGO DOOR AFT END INNER PAN CRACKED AT CARGO DOOR LATCH. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-04, 51-10-03, 51-30-05, AND 52-05, FIGURE 26A.Mar 23, 2000 · N938AS · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000333Fitting · crackedINSPECTION FOUND MID PIT DOOR INTERIOR FITTING JUST AFT OF FORWARD HINGE CRACKED. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-01, 51-10-04, AND 51-30-12.Mar 23, 2000 · N938AS · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000331Frame · corrodedINSPECTION FOUND LONGERON FORMER CORRODED IN AFT CARGO BAY AT STA 1041, LONGERON 29L-30. THE LONGERON FORMER WAS REMOVED AND A NEW LONGERON FORMER WAS INSTALLED IAW SRM 51-30-05 AND 51-10-03.Mar 22, 2000 · N938AS · Doug DC982 · Fuselage Main, FrameSDR CALA0000326Flange · damagedINSPECTION FOUND AFT CARGO DOOR FORWARD AFT LOWER AND UPPER FLANGES DAMAGED AT STOP POSITION. DOUBLERS WERE INSTALLED IAW SRM 51-30-01, 51-30-02, 51-10-03, AND ECRA 5330-02819.Mar 20, 2000 · N938AS · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000325Skin · dentedINSPECTION FOUND THREE SHARP DENTS IN MID CARGO DOOR OUTER SKIN. THE DENTED AREA WAS REPAIRED BY INSTALLING DOUBLERS IAW SRM 53-04, FIGURE 38.Mar 20, 2000 · N938AS · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000324Skin · bentINSPECTION FOUND AFT CARGO DOOR SKIN AROUND HANDLE BENT AND CHAFED. THE DAMAGED AREA WAS CUT OUT IAW SRM 52-05, FIGURE 3. REPAIR DOUBLERS, FILLER, AND SHIMS WERE INSTALLED IAW SRM 52-05.Mar 20, 2000 · N938AS · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000323Floor Support · brokenINSPECTION FOUND SUB FLOOR MEMBRANE BROKEN AT FS 196, LBL 44 JUST FORWARD OF LT O/B SEAT TRACK. THE SUB FLOOR MEMBRANE WAS REPAIRED IAW SRM 53-01, FIGURE 4 AND 51-30-02.Mar 20, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000322Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 146 - 200 JUST LEFT OF CENTERLINE. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-01, 51-10-01, AND 51-10-03.Mar 20, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000321Angle · crackedINSPECTION FOUND LT GILL LINER SUPPORT FRAME CRACKED IN AFT CARGO BAY AT STA 1271. THE SUPPORT ANGLE WAS REMOVED, REPAIRED, AND INSTALLED IAW SRM 51-30-02, 51-10-04, AND 51-30-05.Mar 20, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000319Floor Support · crackedINSPECTION FOUND RT GILL LINER SUPPORT FRAME CRACKED IN AFT CARGO BAY AT STA 1136. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-02, 51-10-04, AND 51-30-05.Mar 20, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000318Floor Support · crackedINSPECTION FOUND AFT CARGO BAY LT UPPER AND LOWER GILL LINER SUPPORT FRAMES CRACKED AT STA 1212. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-30-02 AND 51-30-05.Mar 20, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000317Floor Support · corrodedINSPECTION FOUND RT SIDE FLOOR SUPPORT CORRODED AT STA 180 - 200. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 53-01, FIGURE 1, 51-10-03, 51-30-02, AND 51-30-05.Mar 20, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000316Seat Track · corrodedINSPECTION FOUND RT O/B CABIN SEAT TRACK CORRODED FROM STA 220 - 237. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-02, 51-10-04, 51-10-03, AND 51-30-05.Mar 20, 2000 · N938AS · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000315Shear Tie · corrodedINSPECTION FOUND SHEAR TIE CORRODED IN AFT CARGO BAY AT STA 1231, LONGERON 29L-30. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 51-30-02.Mar 20, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000313Support · corrodedINSPECTION FOUND UPPER AND LOWER SURFACES OF FLOOR SUPPORT ANGLE CORRODED IN AFT CARGO BAY AT STA 1117-1155. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-01, 51-10-04, AND 51-10-03.Mar 18, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000312Angle · chafedINSPECTION FOUND RT MLG DOOR AFT LOWER INNER CORNER REPAIR ANGLE DEEPLY CHAFED. AN INNER CORNER DOUBLER REPAIR WAS INSTALLED IAW SRM 52-05, FIGURE 28, 51-10-04, AND 51-10-03.Mar 18, 2000 · N938AS · Doug DC982 · Landing Gear DoorsSDR CALA0000311Stop · wornINSPECTION FOUND FORWARD CARGO DOOR FORWARD AND AFT LOWER FLANGE AND STOP PADS WORN. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02819.Mar 18, 2000 · N938AS · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000310Stop · wornINSPECTION FOUND MID CARGO DOOR FORWARD AND AFT LOWER FLANGE AND STOP PADS WORN. THE AREAS WERE REPAIRED USING A DOUBLER IAW ECRA 5330-02819 AND SRM 51-10-03.Mar 18, 2000 · N938AS · Doug DC982 · Cargo/Baggage DoorsSDR CALA0000309Frame · crackedINSPECTION FOUND A 3 CRACK IN AFT CARGO BAY RT GILL LINER SUPPORT FRAME AT STA 1041, RBL24. THE ANGLE SUPPORT WAS REMOVED AND A NEW ANGLE SUPPORT WAS INSTALLED IAW SRM 51-30-05 AND 51-10-04.Mar 18, 2000 · N938AS · Doug DC982 · Fuselage Main, FrameSDR CALA0000306Intercostal · corrodedINSPECTION FOUND INTERCOSTAL CORRODED IN AFT CARGO BAY AT STA 1136-1155, LONGERON 29L. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.Mar 15, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0000305Bracket · crackedINSPECTION FOUND LT FORWARD EMERGENCY EXIT DOOR BINDING DUE TO A CRACKED FORWARD SIDE LT BRACKET. THE CRACK WAS 1.5 INCH LONG AND THE BRACKET WAS LOCATED AT FS 864, LONGERON 13L. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-08 AND 5Mar 15, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9901517Strut · deflatedTHE NOSE GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION DEPARTING DEN AND THE AIRCRAFT WOULD NOT PRESSURIZE UNTIL PULLING THE RIGHT GROUND CONTROL RELAY. THE ABNORMAL CHECKLIST WAS COMPLETED AND THE NOSE GEAR LIGHT EXTINGUISHED. THE AIRCRAFT WAS RETURNENov 21, 1999 · N938AS · Doug DC982 · Nose/Tail Landing Gear Strut/AxleSDR CALA9801916Oven · failedAN ELECTRICAL BURNING ODOR WAS NOTICED IN THE FORWARD CABIN AREA WHILE EN ROUTE TO ATL. NO VISIBLE SMIKE WAS PRESENT. THE AIRCRAFT LANDED AT ATL WITHOUT INCIDENT. MAINTENANCE FOUND THE FORWARD GALLEY NR 2 OVEN HAD A BURNED MOTOR. THE OVEN WAS PLACARDED INOPOct 7, 1998 · N938AS · Doug DC982 · Buffet/GalleysSDR CALA9801497Valve · leakingTHE RT HYDRAULIC SYSTEM QUANTITY DECREASED DURING CLIMBOUT. QRH PROCEDURES WERE FOLLOWED FOR HYDRAULIC QUANTITY LOSS AND ALTERNATE GEAR EXTENSION WAS USED FOR RETURN TO MCO WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT INBOARD ANTI-SKIAug 23, 1998 · N938AS · Doug DC982 · Brake Anti-Skid SectionSDR CALA9800991Prox Sensor · inoperativeTHE NOSE GEAR RED LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND THE RED LIGHT EXTINGUISHED. THE FLIGHT WAS CONTINUED TO ORD WHERE IT LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE FOUND THE NLG UPLOCK PROXIMITY SENSOR AT FAULT. THJun 8, 1998 · N938AS · Doug DC982 · Landing Gear Position and WarningSDR CALA9800412Beam · corrodedINSPECTION FOUND MID BAGGAGE BIN Z-ANGLE BEAM CORRODED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 63.Mar 11, 1998 · N938AS · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9800396Doubler · corrodedINSPECTION FOUND NR 2 RADIO ALT RECEIVER ANTENNA RETAINING DOUBLER CORRODED. THE RETAINING DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-00 AND 51-30-2.Mar 5, 1998 · N938AS · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9700054Compressor · damagedTHE AIRCRAFT WAS DIVERTED TO DEN WITH THE NR 1 ENGINE SHUTDOWN WHILE EN ROUTE. THE AIRCRAFT LANDED IN DEN WITHOUT INCIDENT. AN ENGINE CHANGE IS IN PROGRESS. *S/D* INVESTIGATION REVEALED THAT THE ENGINE FAILURE WAS CAUSED BY INGESTION OF BLUE ICE ORIGINATINJan 9, 1997 · N938AS · Doug DC982 · Turbine Engine Compressor SectionSDR ASAA9680208Evac Slide · brokenSEA - PRIOR TO DEPARTURE OF FLIGHT 598 - CREW REPORTED THE R1 DOOR EMERGENCY EVACUATION SLIDE DEPLOY LANYARD WAS BROKEN AND DETACHED. REPLACED THE EMERGENCY EVACUATION SLIDE. (M)Sep 22, 1996 · N938AS · Doug DC982 · Escape SlideSDR ASAA9680082Batteries · dischargedSEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 13 THROUGH 18 WERE FOUND INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY AND LIGHT OPERATED NORMALLY. (M)Mar 28, 1996 · N938AS · Doug DC982 · Emergency LightingSDR ASAA9680081Coalescers · contam checkLAS - FLT NR 9000, AIRCRAFT WAS RELEASED FOR MAINTENANCE FERRY FLIGHT TO SEA (REF MRR ASAA9680080). AFTER TAKEOFF, BOTH PILOTS DETECTED AND ODOR IN THE COCKPIT WHICH MAINTENANCE TECH FOREMAN OCCUPYING THE OBSERVERS SEAT ATTRIBUTED TO A HOT DUCT ODOR. AIRCRAFMar 27, 1996 · N938AS · Doug DC982 · Humidity Control SystemSDR ASAA9680080Tr Return Line · leakingLAS - FLT NR 624 - CREW REPORTED AN ELECTRICAL OR HOT PLASTIC ODOR IN THE CABIN DURING DESCENT AND LANDING. INSPECTION OF ALL LAVATORY WASTE CONTAINERS, OVENS, BUN WARMERS AND COFFEE MAKERS REVEALED NO PLASTIC RESIDUE OR OVERHEAT CONDITION, ODOR HAS DISSIPATEMar 26, 1996 · N938AS · Doug DC982 · Engine Thrust ReverserSDR 96ZZZM700Coalescers · dirtyLAS - FLT NR 624 - CREW REPORTED AN ELECTRICAL OR HOT PLASTIC ODOR IN THE CABIN DURING DESCENT AND LANDING. INSPECTION OF ALL LAVATORY WASTE CONTAINERS, OVENS, BUN WARMERS AND COFFEE MAKERS REVEALED NO PLASTIC RESIDUE OR OVERHEAT CONDITION, ODOR HAS DISSIPATEMar 26, 1996 · N938AS · Doug DC982 · Humidity Control System
Back to N938AS, cancelled Mar 21, 2013