N938MC, cancelled May 9, 2022

Service difficulty reports · 56

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 = 'N938MC' AND deregistration_id = 'N938MC-2022-05-09'
  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 CALA0200248Charger · inoperativeINSPECTION FOUND SECTION OF EMERGENCY LIGHTS NEAR AFT LAV INOPERATIVE. THE CHARGER WAS REPLACED IN AFT LAV IAW CHAPTER 20 AND MM 33-53-00. OPERATIONAL CHECKS WERE GOOD IAW MM 33-53-00.Apr 27, 2002 · N938MC · Doug DC983 · Emergency LightingSDR CALA0200237Channel · corrodedINSPECTION FOUND MAIN BAGGAGE BIN LOWER DOOR JAMB Z-CHANNEL CORRODED AROUND HI SHEARS. THE CHANNEL WAS REPLACED IAW SRM 53-05, FIGURE 63 AND DRAWING #5930481.Apr 24, 2002 · N938MC · Doug DC983 · Fuselage Miscellaneous StructureSDR CALA0200233Web · crackedINSPECTION FOUND TWO .5 INCH CRACKS IN WEB DOUBLER AT AFT SIDE OF AFT CARGO DOOR JAMB AT STA 1212 ABOVE LONGERONS 27R-28R. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5310-03742.Apr 22, 2002 · N938MC · Doug DC983 · Fuselage Miscellaneous StructureSDR CALA0200225Beltframe · crackedINSPECTION FOUND A 1/4" CRACK IN BELTFRAME UPPER FLANGE AT ATTACH POINT WITH LONGERON 2L AT STA 1418. REPAIRED IAW SRM 53-03.Apr 20, 2002 · N938MC · Doug DC983 · Fuselage Main, FrameSDR CALA0200222Longeron · crackedINSPECTION FOUND A 1.125" CRACK IN LONGERON 2R AFT OF BELTFRAME STA 1418. THE CRACKED SECTION OF LONGERON WAS CUT OUT AND A NEW SECTION OF LONGERON AND SPLICE WERE INSTALLED IAW SRM 53-02, FIGURE 17.Apr 20, 2002 · N938MC · Doug DC983 · Fuselage Main, Longeron/StringerSDR CALA0200218Longeron · crackedINSPECTION FOUND A 1.25" CRACK IN LONGERON 2L AFT OF BELTFRAME STA 1418. THE CRACKED SECTION OF LONGERON WAS CUT OUT AND A NEW SECTION AND SPLICE WERE INSTALLED IAW SRM 53-02, FIGURE 17.Apr 19, 2002 · N938MC · Doug DC983 · Fuselage Main, Longeron/StringerSDR CALA0000275Angle · crackedINSPECTION FOUND TAIL COMPARTMENT ANGLE CRACKED JUST TO THE RIGHT OF ESCAPE SLIDE PLATFORM AT FS 1350, LONGERON 27R. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-02, 51-10-02, 51-10-04, 51-10-03, AND 51-30-08.Mar 7, 2000 · N938MC · Doug DC983 · Fuselage Miscellaneous StructureSDR CALA0000274Fitting · corrodedINSPECTION FOUND FORWARD SERVICE DOOR FORWARD AND AFT GIRT BAR FITTINGS CORRODED. THE FITTINGS WERE REMOVED AND REPLACED IAW MM 51-30-01.Mar 7, 2000 · N938MC · Doug DC983 · Emergency EquipmentSDR CALA0000273Skin · crackedINSPECTION FOUND TWO EACH CRACKS IN FLANGES OF DORSAL FIN LE AREA AT LOWER RT SIDE OF ACCESS, FS 1340. THE DORSAL FIN LE WAS REPAIRED IAW AD NR 89-08-10, SERVICE BULLETIN 53-223 (11-5-90), EA 5340-01012, AND ECRA 5330-02936.Mar 7, 2000 · N938MC · Doug DC983 · Vertical Stabilizer, Plate/SkinSDR CALA0000225Channel · crackedINSPECTION FOUND A 3 INCH CRACK IN LT MLG I/B DOOR UPPER L/E CORNER. THE Z-CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-30-02, 51-30-05, AND 51-30-08.Feb 29, 2000 · N938MC · Doug DC983 · Landing Gear DoorsSDR CALA0000224Web · corrodedINSPECTION FOUND LOWER VENTRAL DOOR THRESHOLD WEB AFT OF SEAT RETAINER AT FS 1330, RBL 16 CORRODED. THE CORROSION WAS REMOVED IAW SRM 51-10-03. A DOUBLER WAS INSTALLED IAW SRM 51-10-03 AND 53-05. REMOVED AND REPLACED SEAL IAW SRM 51-30 AND 51-10.Feb 29, 2000 · N938MC · Doug DC983 · Fuselage Miscellaneous StructureSDR CALA0000222Web · corrodedINSPECTION FOUND LOWER CUSP CORRODED AT FS 160-218, LBL 56-62. THE CORRODED AREA WAS REMOVED AND A NEW PART WAS INSTALLED IAW SRM 51-30-02, 51-10-04, 51-10-03, 51-30-05, AND 51-30-07.Feb 29, 2000 · N938MC · Doug DC983 · Fuselage Miscellaneous StructureSDR CALA0000221Frame · corrodedINSPECTION FOUND AFT CARGO DOOR CUTOUT LOWER FRAME CORRODED AT FS 1136-1193, L27R. THE CORROSION WAS REMOVED IAW SRM 51-10-03. A NEW STRAP WAS INSTALLED IAW SRM 53-05, FIGURE 3, 51-10-04, AND 51-10-03.Feb 29, 2000 · N938MC · Doug DC983 · Fuselage Main, FrameSDR CALA0000220Floorbeam · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 160-200, RBL 44. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-04, 53-14-01, AND 51-30-02.Feb 29, 2000 · N938MC · Doug DC983 · Fuselage Main, Floor BeamSDR CALA0000206Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN ATTACH ANGLE AT STA 1418, LONGERON 2L IN TAIL COMPARTMENT CEILING. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-04, 51-10-03, AND 51-30-05.Feb 25, 2000 · N938MC · Doug DC983 · Fuselage Miscellaneous StructureSDR CALA0000205Floorbeam · crackedINSPECTION FOUND FLOOR SUPPORT WEB CRACKED STA 1287-1301, RBL 2. AN INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.Feb 25, 2000 · N938MC · Doug DC983 · Fuselage Main, Floor BeamSDR CALA0000203Intercostal · crackedINSPECTION FOUND THE LOWER ANTI-COLLISION BEACON PANEL ATTACH STRUCTURE CORRODED AND A 3 CRACK IN INTERCOSTAL. THE CORROSION WAS REMOVED AND FOUND WITHIN LIMITS IAW SRM 51-10-03 AND 53-01, FIGURE 1. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTFeb 24, 2000 · N938MC · Doug DC983 · Fuselage Miscellaneous StructureSDR CALA0000202Cargo Track · corrodedINSPECTION FOUND AFT CARGO LEFT TIE DOWN TRACK CORRODED AT FS 1200-1320. THE CARGO TIE DOWN TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-01, 51-30-05, 51-10-04, AND 51-30-03.Feb 24, 2000 · N938MC · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000200Cargo Track · crackedINSPECTION FOUND A 1.5 CRACK IN AFT CARGO PIT RT CARGO TIE DOWN TRACK AT STA 1117. A SECTION OF CARGO TRACK WAS SPLICED IN IAW SRM 53-05, FIGURE 4G.Feb 24, 2000 · N938MC · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000199Angle · corrodedINSPECTION FOUND AFT CARGO BAY GILL LINER SUPPORT Z-ANGLE CORRODED AT RT CARGO TIE DOWN TRACK, STA 1155. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2.Feb 24, 2000 · N938MC · Doug DC983 · Fuselage Miscellaneous StructureSDR CALA0000198Skin · dentedINSPECTION FOUND SKIN OF HORIZONTAL STABILIZER LE OB SECTION IB END DENTED. A DOUBLER WAS INSTALLED IAW EA 9-5513-2-A0602 AND SRM 51-30-2.Feb 24, 2000 · N938MC · Doug DC983 · Horizontal Stabilizer, Plate/SkinSDR CALA0000197Rib · gougedINSPECTION FOUND LEFT ELEVATOR L/E RIB NR 11 GOUGED AND DENTED. THE RIB WAS REMOVED AND A REPAIR ANGLE WAS INSTALLED IAW SRM 51-30-01, 51-10-04, AND 51-10-03.Feb 24, 2000 · N938MC · Doug DC983 · Elevator, Spar/RibSDR CALA0000194Splice · corrodedINSPECTION FOUND SPLICES FOR TIE DOWN AT FS 1212 CORRODED. THE SPLICES WERE REMOVED AND NEW SPLICES WERE INSTALLED IAW SRM 51-30-2 AND 51-10-3.Feb 23, 2000 · N938MC · Doug DC983 · Fuselage Miscellaneous StructureSDR CALA0000193Floorbeam · crackedINSPECTION FOUND FLOOR SUPPORT WEB CRACKED AT STA 1287-1301, BL 0. AN INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.Feb 23, 2000 · N938MC · Doug DC983 · Fuselage Main, Floor BeamSDR CALA0000192Bracket · brokenINSPECTION FOUND TRANSITION ANGLE ATTACH BRACKET BROKEN AT FS 514, LONGERON 23L. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-10-04, 51-10-02, 51-10-03, AND 51-30-01.Feb 23, 2000 · N938MC · Doug DC983 · Fuselage Miscellaneous StructureSDR CALA0000179Skin · crackedINSPECTION FOUND A 4 INCH CRACK IN LEFT MLG I/B DOOR AT LOWER FORWARD CORNER. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW EA 5281-2-A064 AND ECRA 5280-01220.Feb 21, 2000 · N938MC · Doug DC983 · Landing Gear DoorsSDR CALA0000172Skin · gougedINSPECTION FOUND AFT CARGO DOOR LEADING EDGE SKIN GOUGED. THE GOUGED AREA WAS CUT OUT AND A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 52-05, FIGURE 1 AND 51-10-03.Feb 17, 2000 · N938MC · Doug DC983 · Cargo/Baggage DoorsSDR CALA0000171Seat Track · corrodedINSPECTION FOUND RT O/B SEAT TRACK CORRODED AT STA200-245. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-10-04 AND 51-30-05.Feb 17, 2000 · N938MC · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000170Floorbeam · corrodedINSPECTION FOUND G-2 GALLEY FLOOR SUPPORT CORRODED AT FS 218, RBL 6. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-05 AND 51-10-03.Feb 17, 2000 · N938MC · Doug DC983 · Fuselage Main, Floor BeamSDR CALA0000169Floorbeam · corrodedINSPECTION FOUND FLOOR SUPPORTS CORRODED AT FS 160-200, BL 0 TO LBL 12 AND AT STA 200, BL 0 TO RBL 44. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-30-01, 51-30-02, 51-10-04, 51-10-3, AND 53-14-01.Feb 17, 2000 · N938MC · Doug DC983 · Fuselage Main, Floor BeamSDR CALA0000168Seat Track · corrodedINSPECTION FOUND LEFT SEAT TRACK CORRODED AT FS 1098-1285. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-01, 51-10-04, AND 51-10-03.Feb 17, 2000 · N938MC · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0000167Skin · corrodedINSPECTION FOUND SUBFLOOR SKIN AT G-2 GALLEY ALIGNMENT PIN HOLE, STA 218, RBL 6, CORRODED. THE SUB FLOOR SKIN WAS REMOVED AND A FILLER AND DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 2 AND 51-10-03.Feb 17, 2000 · N938MC · Doug DC983 · Fuselage Main, Plate/SkinSDR CALA0000166Web · crackedINSPECTION FOUND CUSP WEB CRACKED AT FASTENER HOLE, STA 245, RBL 45. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 4.Feb 17, 2000 · N938MC · Doug DC983 · Fuselage Miscellaneous StructureSDR CALA0000165Galley Track · corrodedINSPECTION FOUND G-1 GALLEY SUPPORT CORRODED AT FS 160, RBL 40. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-04, 51-20-03, 51-30-02, AND 51-30-05.Feb 17, 2000 · N938MC · Doug DC983 · Fuselage Miscellaneous StructureSDR CALA0000164Angle · corrodedINSPECTION FOUND AFT CARGO DOOR CUTOUT FORWARD LOWER CORNER ANGLE CORRODED. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-20-05.Feb 17, 2000 · N938MC · Doug DC983 · Fuselage Miscellaneous StructureSDR CALA0000163Door Pan · chafedINSPECTION FOUND AFT CARGO DOOR PAN CHAFED UNDER STOPS. REPAIR PARTS WERE INSTALLED IAW ECRA 5330-02819 AND SRM 51-10-03.Feb 17, 2000 · N938MC · Doug DC983 · Fuselage Miscellaneous StructureSDR CALA0000162Door Pan · gougedINSPECTION FOUND FORWARD AND AFT END OF MID CARGO DOOR PAN GOUGED AROUND THE DOOR LATCH ROLLER CAM. REPAIR DOUBLERS WERE INSTALLED IAW SRM 51-10-04, 52-05, FIGURE 26A, 51-10-03, 51-30-05, AND 51-30-02.Feb 17, 2000 · N938MC · Doug DC983 · Fuselage Miscellaneous StructureSDR CALA0000201Fitting · corrodedINSPECTION FOUND G-2 GALLEY FLOOR SUPPORT FITTING CORRODED AT FS 160, RBL 3. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-02 AND 51-30-05.Feb 14, 2000 · N938MC · Doug DC983 · Fuselage Miscellaneous StructureSDR CALA9901239Valve · failedTHE NOSE GEAR RED UNSAFE LIGHT WOULD NOT EXTINGUISH AFTER GEAR RETRACTION. CYCLING THE GEAR PRODUCED NO CHANGE. THE AIRCRAFT WAS RETURNED TO SFO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE STRUT FLAT. THE SHRADER VALVE WAS REPLACED AND THESep 17, 1999 · N938MC · Doug DC983 · Nose/Tail Landing Gear Strut/AxleSDR CALA9900622Power Supply · inoperativeINSPECTION FOUND THE EXTERIOR EMERGENCY EXIT LIGHTS ON BOTH THE RT AND LT SIDE OF AIRCRAFT INOPERATIVE. THE POWER SUPPLY WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD.Jun 2, 1999 · N938MC · Doug DC983 · Emergency LightingSDR CALA9800279Skin · dentedINSPECTION FOUND SEVEN SMALL DENTS 18 INCHES AFT OF LOWER AFT CORNER OF L-1 DOOR NEAR CUSP LINE. AN EDDY CURRENT INSPECTION FOUND NO CRACKS. THE DENTS WERE PLACED ON DIP PER SRM 53-04, PAGE 212, CONDITION 2. THE DIP SPECIFIED INSPECTION EVERY 3500 LANDINGS Feb 20, 1998 · N938MC · Doug DC983 · Fuselage Main, Plate/SkinSDR CALA9800088Connector · looseWHEN GEAR WAS EXTENDED ON FINAL APPROACH TO IAH, THE NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AND THE GEAR WARNING HORN SOUNDED ABOUT FIVE SECONDS LATER. THE GEAR WAS CYCLED AND THE GREEN NOSE GEAR LIGHT ILLUMINATED AND THE WARNING HORN STOPPED 15 SECOJan 21, 1998 · N938MC · Doug DC983 · Landing Gear Position and WarningSDR CALA9700341Skin · impactedTHE JETWAY STRUCK AIRCRAFT AND DAMAGED SKIN AT FORWARD ENTRY DOOR HOLD OPEN AREA STA 119-120. A CLASS III DOUBLER REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 12B. A DIP WAS ISSUED TO REPLACE THE REPAIR WITH A PERMANENT REPAIR WITHIN 8,000 CYCLES AND TO REINSPMar 14, 1997 · N938MC · Doug DC983 · Fuselage Main, Plate/SkinSDR CALA9601604Structure · damagedA LAV SERVICE TRUCK STRUCK THE FUSELAGE 29 INCHES BELOW FORWARD EDGE OF SUGAR SCOOP RESULTING IN DAMAGE TO SKIN AND LONGERON. THE DAMAGED AREA WAS APPROXIMATELY 4 INCHES X 4 INCHES. A CLASS III REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 12B, SHEET 18. A DIOct 31, 1996 · N938MC · Doug DC983 · Fuselage Main, StructureSDR CAL960391Skin · dentedMIA - INSPECTION FOUND 2 DENTS IN EXTERNAL LT FUSELAGE SKIN AT STA 120. THE DENTED AREA WAS REMOVED. REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW ECRA 5330-02363. (X)Feb 26, 1996 · N938MC · Doug DC983 · Fuselage Main, Plate/SkinSDR CAL960392Skin · nickedMIA - INSPECTION FOUND A .50 INCH LONG NICK IN RT FUSELAGE SKIN AT STA 237. THE AREA WAS REPAIRED IAW SRM 53-04, FIGURE 38, SHEET 21. (X)Feb 10, 1996 · N938MC · Doug DC983 · Fuselage Main, Plate/SkinSDR CAL960397Floor Web · corrodedMIA - INSPECTION FOUND CABIN FLOOR WEB CORRODED AT CUSP LINE BETWEEN STA 550 TO STA 560 RIGHT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 4. (X)Feb 7, 1996 · N938MC · Doug DC983 · Fuselage Miscellaneous StructureSDR CAL960396Gusset · crackedMIA - INSPECTION FOUND 1.5 INCH CRACKS IN GUSSET PLATES AT LEFT AND RIGHT SIDES OF KEEL BEAM RIB AT STA 946. THE GUSSET PLATES WERE REMOVED. NEW GUSSET PLATES WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, 51-10-4B, AND 51-30-5. (X)Feb 6, 1996 · N938MC · Doug DC983 · Fuselage Miscellaneous StructureSDR CAL960395Angle · corrodedMIA - INSPECTION FOUND CORROSION IN FLOOR ATTACH ANGLE FROM RT INBOARD FLOOR TRACK TO RT CABIN SIDEWALL AT FS 200. A NEW FLOOR SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-00. (X)Feb 6, 1996 · N938MC · Doug DC983 · Fuselage Miscellaneous StructureSDR CAL960394Web · corrodedMIA - INSPECTION FOUND CORROSION ON CABIN FLOOR HORIZONTAL WEB OUTBOARD OF RT OUBOARD FLOOR TRACK, FS 256. A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-08-00, PAGE 8. (X)Feb 6, 1996 · N938MC · Doug DC983 · Fuselage Miscellaneous Structure
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