N377NW
Service difficulty reports · 165
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 = 'N377NW' AND registry_match = 'registration' 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.
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 = 'N377NW' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DALA2026050302784Hmu · faultyDISCONTINUED TAKEOFF AT LESS THAN 10 KNOTS DUE TO LEFT ENGINE DID NOT ACCEL. HMU CHANGE IN PROGRESS. (LP: 8361006). AIRCRAFT WAS GROUNDEDSDR DALA2026030801591Skin · damagedCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED BTW FR 13 TO FR 14 RH SIDE LEVEL Z=1330 UPPER FUSELAGE (REFERENCE AA CA RD 5100-01821-01A). C/A: COMPLIED WITH ER/A 520355-14 REV.B MATCHES WITH ALL STEPS ON PRI 520355-14 PRI REV 0,1,2,3 ITS SDR DALA2026030801590Window Frame · crackedCRACK INDICATION FOUND ON LH WINDSHIELD CENTER POST LOWER ATTACHMENT A REA, UPPER CORNER RADIUS, CRACK DIRECTION IS HORIZONTAL, CRACK LENGTH IS 0.312 INCH, AD 2020-17-03 / WORKCARD 5311-01226-01. REQUESTING REPA IR DISPOSITION. REPAIR MUST BE ACCOMPLISHED PRIOSDR DALA2026030801589Fitting · damagedPERFORM ER/A 631768-14AD FOR REPLACEMENT OF CONTINUITY FITTINGS LH AND RH ON AREA OF WINSHIELD CENTER POST LOWER ATTACHMENT. COMPLIED WITH ERA 631768-14AD REV. ORIGINAL; MATCHES WITH ALL STEPS ON ER/A 631768-14AD PRI REV.0 AND ER/A 631768-14AD PRI REV1. IT HASDR DALA2026030801588Fitting · damagedPERFORM ER/A 631768-14AD FOR REPLACEMENT OF CONTINUITY FITTINGS LH AND RH ON AREA OF WINSHIELD CENTER POST LOWER ATTACHMENT. C/A: COMPLIED WITH ERA 631768-14AD REV. ORIGINAL; MATCHES WITH ALL STEPS ON ER/A 631768-14AD PRI REV.0 AND ER/A 631768-14AD PRI REV1. ISDR DALA2026031001625Stringer · corrodedCORROSION STRINGER 40L AND FR 29 TO FR 30 IN FWD CARGO COMPARTMENT. PERFORMED REPAIR INSTRUCTION AT STRINGER 40L AND FR 28 TO FR 30 IN FWD CARGO COMPARTMENT IAW SRM 53-21-13-300-018, DWG: D53231712, ISSUE: E00, RELEASE DATE: 28/MAY/98, MEASURES OF CORROSION WSDR DALA2026031001630Skin · corrodedCORROSION EXTERNAL SKIN LOCATED BTW FR 69 TO FR 70 CUT OUT OF DRAIN AND STR 31R TO STR 32R AT LOWER FUSELAGE. COMPLIED WITH ER/A 632109-14 REV. ORIGINAL APPROVED DATE 03-MAR- 26 MATCHES WITH ALL STEPS ON PRI 632109-14 REV 0 IT HAS BEEN VALIDATED. PERFORMED PESDR DALA2026030801592None · noneCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR FRAME 13 RH SIDE AT Z = 1330 IN PASSENGER CABIN (REFERENCE AA CARD 5100-01821-01A). CONFIRMED DT EVALUATION FOR POSSIBLE FCS REPAIR FRAME 13 RH SIDE AT Z = 1330 IN PASSENGER CABIN AND FOUND MEETS THE GENERAL REQUISDR DALA2026031001628Fitting · out of limitsDTE ERA 631653-14AD REV ORIGINAL. REPAIR AT THE MIRROR FITTING & LHS HOLE D1 IS TIME LIMITED, REQUIRING DTE FOLLOW UP PRIOR TO 91,114 TFC. C/A: REVISE AND UPDATE ERA 631653-14AD WITH DTE RESULTS PRIOR TO 91,114 TFC. ASSOCIATED AA 5311-01226 ADDED FOR AC 3277 ASDR DALA2026031001627Window Frame · noneINSPECTION ERA 631653-14AD REV ORIGINAL. WINDSHIELD FRAMING ( AREA 2) REQUIRES FOLLOW UP INSPECTIONS PRIOR TO 58,114 TFC AND EVERY 4,700 FC THEREAFTER. C/A: ACCOMPLISH FOLLOW UP INSPECTIONS PER ERA 631653-14AD, SECTION II , PRIOR TO 58,114 TFC AND EVERY 4,700 SDR DALA2026031001626Fitting · not reportedCONTINUITY FITTINGS REPLACEMENT IS TIME LIMITED, REQUIRING DTE FOLLOW UP PRIOR TO 60,614 TFC. REVISE AND UPDATE ERA 631768-14AD WITH DTE RESULTS PRIOR TO 60,614 TFC ASSOCIATED AA 5311-01226 ADDED FOR AC 3277 ASSOCIATED ER/A 14-631768 ADDED FOR AC 3277. (LP: 1SDR DALA2026030801596Fitting · noneCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR INTERNAL STRUCTURE REINFORCE FITTING LOCATED BTW FR 42 TO FR 43 AND -Y1292 TO -Y 1650.0 TORSION BOX LOWER SHELL IN MAIN WHEEL WELL (REFERENCE AA CARD 5100-01821- 01A). CONFIRMED DT EVALUATION FOR POSSIBLE FCS REPAISDR DALA2026030801595Stringer · noneCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR STRINGER 42L LOCATED BTW FR 55 TO FR 58 IN AFT CARGO COMPARTMENT (REFERENCE AA CARD 5100-0182 1-01A). CONFIRMED DT EVALUATION FOR POSSIBLE FCS REPAIR STRINGER 42L LOCATED BTW FR 55 TO FR 58 IN AFT CARGO COMPARTMENSDR DALA2026030801594Skin · noneSHIP 3277 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN BTW BE AM 1 TO BEAM 2 AND XP 535.3 TO XP 820.6 AFT LOWER CORNER LH FORWARD PASSENGER CREW DOOR 831 REFERENCE AA CARD 5100-01821- 04A-LF. CONFIRMED DT EVALUATION FOR POSSIBLE FCS REPAISDR DALA2026030801593None · noneCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR FRAME 14 RH SIDE AT Z= 1330 IN PASSENGER CABIN (REFERENCE AA CARD 5100-01821-01A). C/A: CONFIRMED DT EVALUATION FOR POSSIBLE FCS REPAIR FRAME #14 RH SIDE AT Z=1330 IN PASSENGER CABIN AND FOUND MEETS THE GENERAL REQSDR DALA2026031001629None · noneDTE ERA 520355-14 REV B. REPAIR PER ERA 520355-14 REV B SECTION V IS LIMITED TO 12 MONTHS FROM REPAIR EMBODIMENT @ 02MAR2026. C/A: REVISE AND UPDATE ERA 520355-14 WITH DTE RESULTS PRIOR TO 02MAR2027. ASSOCIATED ER/A 14-520355 ADDED FOR AC 3277. (LP: 1476200)SDR DALA2026022701384Web · corrodedCORROSION WEB FRAME LOCATED BTW FR 69 TO FR 70 STR 23L IN AFT GALLEY AREA. FINAL REPAIR RESOLUTION: WELL WRITTEN SIGN OFF; REPLACED WEB FRAME LOCATED BTW FR 69 TO FR 70 STR23L IN AFT GALLEY AREA AS PER A320 SRM 51-42-11, A320 SRM 51-72-11, DWG: D53474180, ISSSDR DALA2026022501344Skin · dentedDENT ON EXTERNAL SKIN LOCATED AT FR 3 & 19 INCHES BELOW RH STRINGER, LOWER FUSELAGE. PERFORMED PERMANENT REPAIR ON THE SKIN IAW SRM 53-11-11-300-041, STEP 2.A, FIGURE 001.SDR DALA2026022301261Seat Track · corrodedAIRCRAFT 3277, CORROSION SEAT TRACK -Y765 LOCATED AT FR 20 AT FWD GALLEY AREA (SSI 5 31189). CORRECTIVE ACTION: REPLACED SEAT TRACK -Y765 LOC BETWEEN FR12 TO FR24 AT FWD GALLEY AREA AS PER A320 SRM 51-72-11, AS PER A320 SRM 51-42-11, DWG D53112812. (LP 1463298SDR DALA2026022101251Floor Support · corrodedAIRCRAFT 3277, CORROSION FLOOR SUPPORT +Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLEY AREA (SSI 534147). CORRECTIVE ACTION: REPLACED FLOOR SUPPORT Y1162.5 LOC. BTW FR68 TO FR69 AT AFT GALLEY AREA AS PER SRM 51-42-11, AS PER A320 SRM 51-72-11, DWG: D53472780SDR DALA2026021601062Seat Track · corrodedCORROSION SEAT TRACK +Y765 LOCATED BTW FR 20 TO FR 21 AT FWD GALLEY AREA. REPLACED SEAT TRACK IAW SRM 51-72-11. (LP 1452614)SDR DALA2026021601061Seat Track · corrodedCORROSION SEAT TRACK +Y765 LOCATED BTW FR 64 TO FR 65 AT AFT GALLEY AREA. REPLACED SEAT TRACK IAW SRM 51-72-11 AND SRM 51-42-11. (LP 1452605)SDR DALA2026021601060Floor Support · corrodedCORRODED FLOOR SUPPORT +Y1162.5 LOCATED BTW FR 66 TO FR 68 AT AFT GALLEY AREA. REPLACED FLOOR SUPPORT AT AFT GALLEY AREA IAW SRM 51-42-11, & SRM 51-72-11. (LP 1452595)SDR DALA2026021501048Floor Support · corrodedCORRODED FLOOR SUPPORT -Y765 LOCATED BTW FR 66 TO FR 70 AT AFT GALLEY AR EA (SSI 534147). REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11 SRM 51-72-11 AND DWG 10N01036. (LP 1451289)SDR DALA2026021201028Floor Support · corrodedCORRODED FLOOR SUPPORT, +Y765, BTW FR 66 - 70 IN THE AFT GALLEY AREA. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, SRM 51-42-11, & DWG 10N01036. (LP 1447191)SDR DALA2026021201027Seat Track · corrodedCORRODED SEAT TRACK, +Y1292, BTWN FR 64 - 65 IN THE AFT GALLEY AREA. REPLACED THE SEAT TRACK IAW SRM 51-42-11, SRM 51-72-11, AND DWG 10N01036. (LP 1447183)SDR DALA2026021201026Seat Track · corrodedCORRODED SEAT TRACK, -Y765, BTW FR 64 - 66 IN THE AFT GALLEY AREA. REPLACED THE SEAT TRACK IAW SRM 51-72-11, & SRM 51-42-11, AND DWG 10N01036. (LP 1447149)SDR DALA2026021201025Floor Support · corrodedCORROSION ON THE FLOOR SUPPORT, -Y254, AROUND HOLES BTW FR 16 - 20 IN THE FWD GALLEY AREA. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, SRM 51-72-11, AND DWG D53111462.SDR DALA2026021101013Seat Track · corrodedAIRCRAFT 3277, CORROSION SEAT TRACK -Y1292 LOCATED AT FR 20 AT FWD GALLEY AREA (SSI 531189). REPLACED THE SEAT TRACK -Y1292 LOCATED BTW FR12 TO FR24 IAW SRM 51-42-11, & SRM 51-72-11.SDR DALA2026020700888Web · corrodedCORRODED WEB FRAME BTW FR 69 TO FR 70, STR 23R IN AFT GALLEY AREA. REPLACED WEB FRAME IAW SRM 51-42-11, SRM 51-72-11, DWG D53474180, ISSUE AA, MEASUREMENT OF CORROSION: L=0.779 IN. W=1.421 IN. L=0.292 IN, W=1.125 IN. (LP 1439399)SDR DALA2026020700887Dummy Rail · damagedMISSING MATERIAL ON RAIL DUMMY Y503.2 LOCATED BTW FR 12 TO FR 16 IN FWD GALLEY AREA. REPLACED RAIL DUMMY Y503.2 LOCATED BTW FR 12 TO FR 16 AT FWD GALLEY AREA IAW SRM 51-42-11, SRM 51-72-11, DWG D53110984, AND DWG D53112825 , MEASUREMENT OF DAMAGE: L= 1.483SDR DALA2026020700886Shear Plate · corrodedCORROSION SHEAR PLATE, STRINGER 23L, FR 69 - 70 IN THE AFT GALLEY AREA. REPLACED SHEAR PLATE IAW SRM 51-42-11, SRM 51-72-11, & DWG D53474180, ISSUE AA, MEASUREMENT OF AREA: L= 2.820 INCHES, W= 2.210 INCHES, D= 0.073, (LP: 1439385)SDR DALA2026020600855Floor Support · corrodedCORROSION FLOOR BEAM -Y1162.5 LOCATED BTW FR 66 TO FR 68 AT AFT GALLEY AREA (SSI 534147). REPLACED FLOOR BEAM -Y1162.5 LOCATED BTW FR 66 TO FR 68 AT AFT GALLEY AREA AS PER A320 SRM 51-72-11 AND A320 SRM 51-42-11. DWG D53472172 RELEASE DATE 24.NOV.22 ISSUE K. SDR DALA2026020600854Shear Plate · corrodedCORROSION LOC. BTW FR69 TO 70 SHEAR PLATE STR 23 R AT AFT GALLEY AREA (EACH). REPLACED SHEAR PLATE LOC. BTW FR69 TO FR70 STR 23 R AT AFT GALLEY AREA AS PER A320 SRM 51-42-11, A320 SRM 51-72-11 AND DWG D53474180 RELEASE DATE: 09/SEP/24 ISSUE: AA TOOK MEASURE OSDR DALA2026020600853Support · corrodedCORROSION LOWER SILL LOCATED AT FR 66 LH SIDE AT AFT GALLEY AREA (SSI 534147). REWORKED CORROSION AS PER SRM A320 51-74-00 AND EVALUATED REWORKED AREA ON LOWER SILL LOC. AT FR66 LH SIDE AT AFT GALLEY AREA AND FOUND WITHIN LIMITS AS PER A320 SRM 53-41-14-283-0SDR DALA2026020200749Strap · crackedCRACKED STRAP ASSY, HINGE FITTING 5 ON THE RT HORIZONTAL STAB. REPLACED THE STRAP ASSY AIW SRM 51-72-11, DWG D55181526, & AMM 55-16-42-400-001-A. MEASUREMENT OF CRACK: L= 0,7170 INCH. (LP 1430773)SDR DALA2026020200748Floor Support · corrodedCORRODED FLOOR SUPPORT -Y1162.5, BTWN FR 68 TO FR 69 AFT GALLEY. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND SRM 51-42-11, AND DWG D53472189, AND DWG D53472780. MEASUREMENT OF CORROSION: L= 0.850 INCH W= 0.668 INCH D= 0.036 INCH.SDR DALA2026020200747Seat Track · corrodedCORRODED SEAT TRACK +Y1292, FR 16 & 20 IN THE FWD GALLEY. REPLACED THE SEAT TRACK IAW SRM 51-72-11, SRM 51-42-11, DWG D53110920. & DWG D53112812. MEASUREMENT OF CORROSION: L= 3.640 IN W= 0.410 IN D= 0.035, (LP 1430750)SDR DALA2026020200741Fitting · corrodedCORROSION CENTER FITTING LOCATED BTW FR 66 TO FR 68 RH SIDE LOWER SILL AT AFT GALLEY AREA (SSI 534147). REPLACED CENTER FITTING LOC. BTW FR 66 TO FR 68 RH SIDE LOWER SILL AT AFT GALLEY AREA IAW SRM 51-42-11, A320 SRM51-72- 11, DWG D53480505, ISSUE: FE. MEASSDR DALA2026020200744Hinge Arm · wornWEAR ON HINGE ARM 5 ELEVATOR ON RH HORIZONTAL STABILIZER. C/A: REPLACED HINGE ARM 5 ELEVATOR ON RH HORIZONTAL STABILIZER IAWAMM 55-16-42-000-001-A, & AMM 55-16- 42-400-001-A. (LP: 1429575)SDR DALA2026020200743Fitting · wornWEAR ON HINGE ARM FITTING 2 AT HORIZONTAL STABILIZER RH SIDE ( 1E/A) (REFER TO AMDS CARD 2734-4001-RT RII). REPLACED HINGE ARM FITTING NR 2 AT HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. (LP 1429561)SDR DALA2026020200742Seat Track · corrodedCORROSION ON SEAT TRACK -Y1292 LOCATED BTW FR 64 TO FR 66. REPLACED THE SEAT TRACK IAW SRM 51-42-11, SRM 51-72-11, DWG 10N01036 ISSUE C, MEASUREMENT OF CORROSION: D=0.0325 INCH. (LP 1428059)SDR DALA2026013000730Floor Support · corrodedCORROSION LOWER SILL LOCATED AT FR 68 LH SIDE AT AFT GALLEY AREA (SSI 534147). PERFORMED PERMANENT REPAIR LOC. ON LOWER SILL AT FR 68 LT SIDE AT AFT GALLEY AREA IAW SRM 53-41-14-300-001; PARAGRAPH 2 .A; FIGURE 001; PRINCIPLE 7. MEASURES OF CORROSION ARE: P1 =SDR DALA2026013000729Fitting · corrodedCORROSION CENTER FITTING LOCATED BTW FR 16 TO FR 20 LH SIDE CUT OUT AT FWD GALLEY AREA (SSI 531189). REPLACED CENTER FITTING LOC. BTW FR 16 TO FR 20 LH SIDE CUT OUT AT FWD GALLEY AREA AS PER A320 SRM 51-42-11, A320 SRM 51-72-11 AND DWG D53112109 RELEASE DATE:SDR DALA2026012900710Floor Support · corrodedCORRODED FLOOR SUPPORT FR 16 & FR 20, Y 254 FWD GALLEY AREA. REPLACED THE FLOOR SUPPORT Y254 BTWN FRS 12 - 24 IAW SRM 51-72-11, SRM 51-42-11, & DWG D53112816 ISSUE G00, DWG D53135202 & DWG D5311092. MEASUREMENT OF CORROSION: P.1 L= 0.720 IN; W= 0.336 IN; SDR DALA2026012900709Support · corrodedCORRODED LOWER SILL, FR 68 RT AT AFT GALLEY AREA. PERFORMED REPAIR INSTRUCTIONS ON LOWER SILL LOCATED AT FR 68 RT IAW SRM 53-41-14-300-001; PARAGRAPH 2.A; FIGURE 001; PRINCIPLE 7. MEASUREMENT OF REWORK ARE L = 6.589 IN, W= 1.481 IN. (LP: 1424365)SDR DALA2026013000731Strut · corrodedCORROSION ON INTERCONNECT STRUT R/H WING (REFERENCE RII AMDS CARD 2751 -9202). REMOVED INTERCONNECT STRUT R/H WING P/N: D5757032201100 S/N: 03620 ON UNSERVICEABLE CONDITION AS PER A320FAM AMM 27-51-44-000 -001-A. REPLACED INTERCONNECT STRUT R/H WING AS PER A3SDR DALA2026012700613Strut · corrodedCORROSION ON INTERCONNECT STRUT LT WING. REFERENCE RII AMDS CARD 27 51-9202. REMOVED INTERCONNECT STRUT LT WING ON UNSERVICEABLE CONDITION IAW AMM 27-51-44-000 -001-A. REPLACED THE INTERCONNECT STRUT LT WING IAW AMM 27-51-44 -000-001-A & INSTALLATION TO SDR DALA2025113008736Window · failedCA SIDE WINDOW BUBBLING AT THE BOTTOM AND EXTREMELY HOT - BURN YOUR HAND HOT. ALSO RECEIVED L WNDW HEAT CAUTION. REMOVED AND REPLACED CAPT SLIDING WINDOW PER A320 AMM 56-12. OPS CHECK GOOD, OK FOR SERVICE. (LP: 7966749)SDR DALA2025092907025Engine · bird ingestionBIRD STRIKE NR 1 ENGINE TOP OF LEADING EDGE. SMALL FLOCK OF SMALL BIRDS NO ENGINE FLUCTUATION NO TEMP CHANGE. INSPECTED NR 1 ENGINE AND FOUND FEATHERS & BLOOD IN CORE 592343 WIP. PER A320 AMM 72-00-00-200-006-A INSPECTED ENG #1 NO VISUAL DAMAGE TO FAN BLADE
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