N13891, cancelled May 12, 2003

Service difficulty reports · 59

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 = 'N13891' AND deregistration_id = 'N13891-2003-05-12'
  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 CALA0100877Support · crackedINSPECTION FOUND A 1.52 INCH CRACK IN NR 1 PYLON UPPER SUPPORT ANGLE AT CANTED FRAME 1463, L17L. A REPAIR ANGLE WAS INSTALLED IAW ECRA 5410-01555.Sep 15, 2001 · N13891 · Doug DC982 · Nacelle/Pylon, Main FrameSDR CALA0001524Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN WEB SKIN JUST FORWARD OF TRIM AT TAIL COMPARTMENT STA 1485, RT SIDE. THE AFT ACCESSORY VENT RT BOX WAS REMOVED IAW SRM 51-30-1. THE REPAIR DOUBLER WAS REMOVED AND A NEW REPAIR DOUBLER WAS INSTALLED IAW SRM 51-30-2, 53-01, FOct 9, 2000 · N13891 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0001523Web · corrodedINSPECTION FOUND CUSP WEB CORRODED AT STA 195, LBL 22-LBL 44. THE CORRODED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 1 AND 51-30-2.Oct 9, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001522Beam · corrodedINSPECTION FOUND LEFT LAV I/B FORWARD AFT BEAM ON FLOOR BENT AND CORRODED AT FORWARD END. THE LAV BEAM WAS REMOVED AND A NEW BEAM WAS INSTALLED IAW 51-10-2, 51-10-3, AND 51-30-1.Oct 9, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001507Skin · dentedINSPECTION FOUND THE LEFT FUSELAGE SKIN DENTED AT STA 389 - 436, LONGERON 22L. REPAIRED IAW ECRA 5331-01082 AND EA 9-5331-2-A0754.Oct 6, 2000 · N13891 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0001492Web · tornCUSP WEB TORN FS 214 AT RBL 10 TO RBL 14. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51-30-8.Oct 5, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001491Seat Track · corrodedRIGHT INBOARD SEAT TRACK CORRODED AT STATION 200 TO 266. REMOVED AND REPLACED SEAT TRACK SECTION PER SRM 51-30-1, 51-30-2, 51-30-5, 53-05 FIG 4F AND 51-10-4.Oct 5, 2000 · N13891 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0001490Skin · dentedEXTERIOR SKIN DENTED AT STATION 265 AT LONGERON 20R. REWORKED DENT. FABRICATED AND INSTALLED DOUBLER PER SRM 53-04 FIG 38 AND 51-30-2.Oct 5, 2000 · N13891 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0001489Floor Support · corrodedFLOOR SUPPORT CORRODED AT STATION 256 CENTER. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-30-5 AND 53-14-2 FIG 4 SHEET 1.Oct 5, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001488Skin · dentedAFT CARGO DOOR SKIN CENTER AFT IS DENTED. REMOVED DAMAGED AREA. REPAIRED SKIN PER SRM 51-50-1 FIG 1 AND 52-05 FIG 3.Oct 5, 2000 · N13891 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0001487Skin · dentedLEFT EXTERIOR SKIN DENTED AT STA 200 BETWEEN LONG 22L AND 23L. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-04 AND 51-10-4.Oct 5, 2000 · N13891 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0001486Longeron · crackedTAIL COMPARTMENT STA 1446 LONG 6R IS CRACKED 1 INCH. REMOVED CRACKED LONGERON. FABRICATED AND INSTALLED NEW LONGERON PER SRM 53-02, 51-10-4 AND 51-10-3.Oct 5, 2000 · N13891 · Doug DC982 · Fuselage Main, Longeron/StringerSDR CALA0001485Cargo Track · corrodedMID PIT RT AFT TRACK SECTION FORWARD END OUTBOARD EDGE CORRODED. REMOVED DAMAGED SECTION. FABRICATED AND INSTALLED NEW SECTION OF TRACK PER SRM 51-10-3, 53-01, 51-10-4, 51-30-1, AND 51-30-2.Oct 5, 2000 · N13891 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0001432Floor Support · corrodedSTA 200 LBL 12 FLOOR SUPPORT IS CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 1-30-5.Sep 26, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001431Floor Support · corrodedSTA 200 RBL 10 - RBL 46 FLOOR SUPPORT HAS ELONGATED HOLES AND CORROSION. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-30-5.Sep 26, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001424Web · puncturedINSPECTION FOUND SUB FLOOR PUNCTURED AT FS 170, RBL 15.5, 21, 26, 36, AND 41. THE PUNCTURED AREAS WERE CUT OUT IAW SRM 53-01, FIGURE 1. A DOUBLER WAS INSTALLED AT EACH LOCATION IAW SRM 53-14-1, FIGURE 4, 51-30-4, 51-10-3, AND 51-30-2.Sep 21, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001423Web · corrodedINSPECTION FOUND CUSP WEB CORRODED AT FS 1076 - 1086, RBL 58. THE FASTENERS AND FRAME FITTINGS WERE REMOVED FROM AROUND THE CORRODED AREA AND THE CORRODED AREA WAS CUT OUT. A REPAIR WEB AND FRAME FITTING WERE INSTALLED IAW SRM 51-30-2, 53-14-3, 51-10-3, AND Sep 21, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001422Web · crackedINSPECTION FOUND A 5 INCH CRACK IN CUSP WEB AT FS 886, LBL 50. THE CRACK WAS STOP DRILLED IAW SRM 53-01, FIGURE 2. A DOUBLER WAS INSTALLED IAW SRM 53-01, 51-10-4, AND 51-20-0.Sep 21, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001426Structure · dentedUPPER AFT EMERGENCY WALKWAY DENTED AT AFT SECTION AFT OF EXIT PAINT. CUT OUT DAMAGED SECTION PER SRM 53-01 FIG 2. VERIFIED NO CRACKS PAST CUTOUT AREA. FABRICATED AND INSTALLED DOUBLER PER SRM 53-01 FIG 2.Sep 18, 2000 · N13891 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0001413Channel · corrodedINSPECTION FOUND AFT VENTRAL DOOR THRESHOLD AREA UNDER FLOOR L-CHANNEL CORRODED AT FS 1338. SUPPORT ANGLES WERE REMOVED AND REPLACED IAW SRM 51-10-4 AND EA 9-5320-2-A0765.Sep 18, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001401Skin · gougedINSPECTION FOUND LT WING NR 5 SLAT LOWER SKIN GOUGED AT I/B END. A DOUBLER WAS INSTALLED IAW SRM 57-03, FIGURE 4, 51-10-3, AND 51-30-8.Sep 6, 2000 · N13891 · Doug DC982 · Leading Edge DevicesSDR CALA0001396Floorbeam · corrodedINSPECTION FOUND LT LAV FLOORBEAM BOLT HOLES CORRODED AT FS 1338. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-10-3, 51-30-05, 51-30-02, AND EA 9-5321-2-A0762.Sep 5, 2000 · N13891 · Doug DC982 · Fuselage Main, Floor BeamSDR CALA0001395Stop · crackedINSPECTION FOUND A 2 INCH CRACK IN BOTH THE AFT AND FWD LOWER DOOR STOPS ON FWD CARGO DOOR. THE CRACKS WERE STOP DRILLED IAW SRM 52-03. DOUBLERS WERE INSTALLED AT EACH LOCATION IAW SRM 51-10-4, 51-10-3, 51-30-2, 51-30-7, 52-03, FIGURE 8, AND ECRA 5230-01554.Sep 5, 2000 · N13891 · Doug DC982 · Cargo/Baggage DoorsSDR CALA0001394Web · crackedINSPECTION FOUND THREE .5 INCH CRACKS IN SUBFLOOR BETWEEN FS 150 AND 168, LBL 22. THE CRACKED AREA WAS REMOVED IAW SRM 53-01, FIGURE 1. A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-4, 51-10-3, AND 51-30-0.Sep 4, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001463Support Bracket · chafedFORWARD FUSELAGE STATION 37 RIGHT HAND PAN SUPPORT HAS DEEP CHAFE. REMOVED AND REPLACED SUPPORT, FABRICATED AND INSTALLED DOUBLER PER SRM 53-01 FIG 1, 51-30-2, 53-02-2 FIG 2 AND 51-10-4.Aug 30, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001335Skin · damagedINSPECTION FOUND LT FUSELAGE EXTERIOR SKIN CREASED AT STA 218 BETWEEN LONGERON 18L AND 19L. THE CREASED AREA WAS CUT OUT IAW SRM 53-04, FIGURE 25. A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 51-10-3, 51-30, 51-30-5, AND 53-04, FIGURE 25.Aug 28, 2000 · N13891 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA0001459Seat Track · corrodedRT HAND OUTBOARD SEAT TRACKS STA 1125 - 1200 IS CORRODED OUT OF LIMITS. REMOVED SECTION OF SEAT TRACK FROM STA 1125 - 1230 IAW SRM 53-05 FIG 4, RECEIVED SEAT TRACK ON TRAVELLER T9021, DRILLED AND LOCATED IAW SRM 51-10-4, TREATED AND PRIMED SEAT TRACK AND SPLIAug 22, 2000 · N13891 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA0001305Web · crackedINSPECTION FOUND A 6 INCH CRACK IN CUSP WEB AT FS 886, RBL 44 - 45. THE CRACKED AREA WAS CUT OUT AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 2A, 51-10-3, AND 51-30-2.Aug 22, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001447Web · puncturedSUB FLOOR PUNCTURED APPROX FS 170 - RBL 10. CUT OUT DAMAGED AREA IAW SRM 53-01 FIG 1. FABRICATED DOUBLER IAW SRM 53-14-1 FIG 4. LOCATED AND DRILLED IAW SRM 51-30-4. TREATED AND PRIMED IAW SRM 51-10-3. INSTALLED IAW SRM 51-30-2.Aug 18, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001453Web · crackedRIGHT HAND CUSP WEB FS 245 AT RBL 44 CRACKED (.5 INCH) AND PUNCTURED. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 2, 51-10-3, AND 51-30-2.Aug 17, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001446Web · crackedRT SIDE CUSP WEB FS 245 APPROX RBL 44 CRACKED AND PUNCTURED. CUT OUT PUNCTURED PER SRM 53-01 FIG 2, FABBED REPAIR DOUBLER PER SRM 53-01 FIG 2, TREATED AND PRIMED PER SRM 51-10-3, INSTALLED PER SRM 51-30-2.Aug 17, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001458Web · corrodedCUSP WEB HEAVILY CORRODED AT FS 224 APPROX LBL 58. FABRICATED CUSP WEB AT FAB SHOP ON TRAVELLER T9073. TREATED AND PRIMED IAW SRM 51-10-3, LOCATED AND TRIMMED AND DRILLED IAW SRM 51-10-4, TO BE INSTALLED ON NR 6215847 ZONE 020 SEQ 0047.Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001457Floor Support · corrodedSTA 160 - 195 LBL 54 FLOOR SUPPORT IN FWD ENTRY IS CORRODED BEYOND LIMITS. REMOVED FLOOR SUPPORT ON TRAVELLER T8983, FOUND CORROSION ON SUB FLOOR. REMOVED CORROSION IAW SRM 51-0-3, SUB FLOOR OUT OF LIMITS. SEE ATTACHED 44.0008 MAT ID 7075-T6.020/BATCH 00001Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001456Floor Support · corrodedSTA 148 - 200 RBL 54 FLOOR SUPPORT CORRODED BEYOND LIMITS (FWD ENTRY). REMOVED FLOOR SUPPORT IAW SRM 51-10-2, RECEIVED NEW FLOOR SUPPORT TRAVELLER T9012, TREATED AND PRIMED IAW SRM 51-10-3, DRILLED FLOOR SUPPORT IAW SRM 51-10-4, INSTALLED SUPPORT IAW SRM 51-3Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001455Web · corrodedCUSP WEB HEAVILY CORRODED AT FS 224 APPROX LBL 58. FABRICATED CUSP WEB AT FAB SHOP ON TRAVELLER T9073, TREATED AND PRIMED IAW SRM 51-10-3, LOCATED, TRIMMED AND DRILLED IAW SRM 51-10-4, TO BE INSTALLED ON NR 6215847 ZONE 020 SEQ 0047.Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001454Skin · gougedRIGHT AILERON LOWER SURFACE SKIN IS GOUGED (.5 INCH) AT LEADING EDGE 18 INCHES OUTBOARD OF DAMPERS. REMOVED AILERON IAW MD-80 MM 27-10-01, REPAIRED AILERON IAW MD-80 SRM 57-01 FIG 5 SHEET 2, PERFORMED WEIGHT AND BALANCE IAW SRM 57-50-01, WEIGHT AND BALANCE ISAug 15, 2000 · N13891 · Doug DC982 · AileronsSDR CALA0001452Floorbeam · corrodedFLOORBEAM CORRODED AT STA 218 LBL 10 - RBL 10. REMOVED AND REPLACED FLOORBEAM PER SRM 51-30-2, 51-10-4, 51-10-3, AND 51-30-5.Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Main, Floor BeamSDR CALA0001451Floor Support · corrodedFLOOR SUPPORT CORRODED IN FORWARD ENTRY AREA STA 160 - 195 LBL 54. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-30-2, AND 51-10-03.Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001450Floorbeam · corrodedFLOORBEAM CORRODED AT FORWARD ENTRY STA 168 RBL 9 - RBL 43. REPLACED FLOORBEAM PER SRM 51-10-04, 51-30-03, 51-30-2, AND 51-30-5.Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Main, Floor BeamSDR CALA0001449Floorbeam · corrodedFLOORBEAM ELONGATED HOLES AND CORROSION AT STA 160 LBL 5 - RBL 5. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED BEAM PER SRM 51-30-5, 51-10-4, AND 51-10-3.Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Main, Floor BeamSDR CALA0001448Floor Support · corrodedSTA 148 - 200 RBL 7 FLOOR SUPPORT CORRODED OUT OF LIMITS FWD ENTRY. REMOVED FLOOR SUPPORT IAW SRM 51-10-2, RECEIVED NEW PART ON TRAVELLER T9013, LOCATE AND DRILL HOLES IAW SRM 51-10-4, INSTALLED FLOOR SUPPORT IAW SRM 51-30-1.Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001445Skin · gougedRT AILERON LWR SURFACE SKIN IS GOUGED AT L/E APPROX 18 INCHES O/B OF DAMPERS. REMOVED AILERON IAW MD-80 MM 27-10-01. REPAIRED AILERON IAW MD-80 SRM 57-01 FIG 5 SHEET 2, PERFORMED WEIGHT AND BALANCE IAW SRM 57-50-01, WEIGHT AND BALANCE IS WITHIN LIMITS. INSAug 15, 2000 · N13891 · Doug DC982 · AileronsSDR CALA0001444Floorbeam · corrodedSTA 218 LBL 10 - RBL 10 FLOORBEAM OUT OF LIMITS FWD ENTRY. REMOVED FLOOR SUPPORT IAW SRM 51-30-2, RECEIVED NEW FLOORBEAM ON T9010, LOCATED AND DRLLED IAW SRM 51-10-4, TREATED AND PRIMED IAW SRM 51-10-3, INSTALLED FLOORBEAM IAW SRM 51-30-5.Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Main, Floor BeamSDR CALA0001443Floor Support · corrodedSTA 195 - 200 LBL 17 FLOOR SUPPORT IS CORRODED OUT OF LIMIT (FWD ENTRY). REMOVED FLOOR SUPPORT IAW SRM 51-30-2, ROUTED TO FAB SHOP, RECEIVED NEW FLOOR SUPPORT ON TRAVELLER T8982, FINISHED FAB PER SAMPLE PER TRAVELLER T8982, INSTALLED IAW SRM 51-30-2.Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001442Floorbeam · corrodedSTA 200 LBL 5- FLOORBEAM IS CORRODED OUT OF LIMITS FWD ENTRY. REMOVED BEAM FOUND TO BE OUT OF LIMITS, FAB NEW BEAM ON T8981, TREATED AND PRIMED IAW SRM 51-10-3, DRILLED AND INSTALLED IAW SRM 551-30-2.Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Main, Floor BeamSDR CALA0001441Floor Support · corrodedSTA 148 - 200 LBL 7 FLOOR SUPPORT IS CORRODED BEYOND LIMITS FWD ENTRY. REMOVED FLOOR SUPPORT AND ROUTED TO FAB (REMOVAL PER SRM 51-30-2) RECEIVED FROM FAB-FABBED PER SAMPLE ON TRAVELLER T-8977, INSTALLED SUPPORT IAW SRM 51-30-2.Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001440Floorbeam · corrodedSTA 168 LBL 16-BLL 38 FLOORBEAM HAS CORROSION FWD ENTRY. REMOVED FLOORBEAM IAW SRM 51-30-2, SENT TO FAB SHOP FOR NEW FLOORBEAM, TREATED AND PRIMED IAW SRM 51-10-3, LOCATED AND DRILLED FLOOR SUPPORT IAW SRM 51-10-3, LOCATED AND DRILLED FLOOR SUPPORT IAW SRM 51Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Main, Floor BeamSDR CALA0001439Floor Support · corrodedSTA 160 - 195 LBL 44 FLOOR SUPPORT IS CORRODED AND HAS ELONGATED HOLES FWD ENTRY. REMOVED FLOOR IAW SRM 51-30-2, FLOOR SUPPORT, FABBED ON TRAVELLER T-8979, DRILLED FLOOR SUPPORT IAW SRM 51-10-4, TREATED AND PRIMED IAW SRM 51-10-2, INSTALLED FLOOR SUPPORT IAW Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0001438Floor Support · corrodedSTA 160 - 200 RBL 44 FLOOR SUPPORT OUT OF LIMITS FWD ENTRY. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-30-5, RECEIVED FLOOR SUPPORT FROM TRAVELER T9018, LOCATED AND DRILLED SUPPORT IAW SRM 51-10-04.Aug 15, 2000 · N13891 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9900123Oil Syst · overservicedA MODERATE AMOUNT OF SMOKE APPEARED IN THE COCKPIT AND CABIN AFTER TAKEOFF FROM EWR WITH THE PNEUMATIC PRESSURE GAUGE READING 70 PSI. THE SMOKE SLOWLY DISSIPATED AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED BOTFeb 14, 1999 · N13891 · Doug DC982 · APU Oil System
Back to N13891, cancelled May 12, 2003