Boeing 737-277
Service difficulty reports · 1,584
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = '737277' 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 aircraft_model_key = '737277' 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 AWXA0002208Web · crackedD: Frame web cracked 3 ea places at fastener holes, BS 639, RBL 65, WL 206C: Removed cracked web, drilled and installed new web IAW B737 200 SRM 51-40-2 at BS 639, RBL 65, wl 206SDR AWXA200100468Skin · chafedMCN - C21 CK - C - LT WING, I/B FLIPPER FLAP LOWER O/B SKIN CHAFED BEYOND LIMITS. MAINTENANCE REMOVED THE LOWER SKIN PANEL, FABRICATED AND INSTALLED NEW LOWER SKIN PANEL IAW AWA ER 15-5752-01249-DL4.SDR AWXA200100464Stiffener · crackedMCN - C21 - C - BS 178 PRESS BULKHEAD WEB, AFT SIDE, VERT TEE CRACKED 1 INCH ON I/B SIDE, WL 184 TO 185, LBL 5.7, FOUND VISUALLY AND CONFIRMED BY HFEC. MAINTENANCE CUT OUT DAMAGED AREA OF VERT TEE AND FORMED REPAIR ANGLES, STRAPS AND FILLERS AND INSTALLED REPSDR AWXA200100457Bulkhead · crackedC21 CK - C - AFT SIDE OF BS 178 PRESS BULKHEAD CENTER WEB HAS A .5 INCH CRACK AT LBL .7, WL 203 TO 203.5, CONFIRMED WITH HFEC. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLERS AND INSTALLED REPAIR IAW B737 SRM 53-10-11, PG 83 & 84 AND TSDR AWXA200100469Floorbeam · corrodedMCN - C21 CK - C - BS 967 FLOORBEAM UPPER FLANGE CORRODED IN 4 PLACES BETWEEN LBL 22 AND RBL 49, BEYOND SRM LIMITS. MAINTENANCE REMOVED THE FLOORBEAM UPPER CAP AND FABRICATED AND INSTALLED NEW UPPER CAP IAW B737 SRM 53-10-9, FIG 2, PG 7 - 11.SDR AWXA200100467Floorbeam · corrodedMCN - C21 CK - C - FLOORBEAM BS 986.5, LBL 44 TO RBL 49 HAS CORROSION IN SEVERAL PLACES ON UPPER FLANGE. MAINTENANCE REMOVED THE FLOORBEAM UPPER CAP FROM LBL 44 TO RBL 49 AND FABRICATED NEW UPPER CAP SECTION AND INSTALLED IAW B737 SRM 53-10-9 FIG 2 PG 7 - 11.SDR AWXA200100471Frame · crackedMCN - C21 CK - C - BS 178 PRESS BULKHEAD 1.7 INCH CRACK CENTER OF RADIUS, RT CHORD, WL 207, RBL 24. MAINTENANCE REMOVED AND REPLACED THE RT SIDE CHORD IAW AWA ER 15-5311-01242-TB2.SDR AWXA200100470Web · crackedMCN - C21 CK - C - RT COCKPIT FLOOR WEB CRACKED 1 INCH AT CUTOUT, BS 180, WL 207, RBL 24. MAINTENANCE REMOVED THE FLOOR WEB, FABRICATED AND INSTALLED NEW FLOOR WEB IAW AWA ER 15-5311-01234-TR1.SDR AWXA200100466Bulkhead · crackedMCN - C21 CK - C - BS 178 PRESS BULKHEAD CENTER WEB HAS A 1 INCH CRACK, WL 227.7 TO 228.7, RBL 6.4, BELOW REINFORCEMENT, FOUND WHILE PERFORMING ULTRASONIC INSPECTION. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED REPAIR SDR AWXA200100465Bulkhead · crackedMCN - C21 CK - C - BS 178 PRESS BULKHEAD CENTER WEB .7 INCH CRACK, WL 218, RBL 11.7 TO RBL 12.7, BELOW REINFORCEMENT DETECTED BY ULTRASONIC INSPECTION. MAINTENANCE CUT OUT DAMAGED AREA OF WEB AND FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED IAW B737 SRMSDR AWXA200100460Bulkhead · crackedMCN - C21 CK - C - BS 178 PRESS BULKHEAD CENTER WEB HAS A 1 INCH CRACK AT LBL 6.6, WL 221.5 TO WL 222.5 BELOW REINFORCEMENT AS DETERMINED WITH ULTRASONIC INSPECTION. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLERS AND INSTALLED REPAIRSDR AWXA200100459Bulkhead · crackedMCN - C21 CK - C - BS 178 PRESS BULKHEAD CENTER WEB HAS A .8 INCH CRACK AT LBL 9.2 TO LBL 10, WL 218, UNDER REINFORCEMENT AS DETERMINED WITH ULTRASONIC INSPECTION. MAINTENANCE CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND FILLERS AND INSTALLED REPAIR IASDR AWXA200100454Skin · crackedC-21 CK - C - L-1 DOOR CUTOUT FUSELAGE SKIN LOWER EDGE BS 338.5 CRACKED .0625 INCH AT SILL PLATE ATTACH HOLE. MAINTENANCE REAMED CRACKED FASTENER HOLE, DRILLED AND INSTALLED REPAIR DOUBLER AT L-1 DOOR CUTOUT LOWER EDGE, BS 338.5 PER AWA ER 15-5300-01234-DD1.SDR AWXA200100463Bulkhead · crackedMCN - C21 CK - C - BS 178 PRESS BULKHEAD CENTER WEB HAS A .75 INCH CRACK, WL 234, RBL 10, FWD SIDE AT A FASTENER HOLE, AS DETERMINED WITH HFEC. MAINTENANCE CUT OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED IAW B737 SRM 53-10-11, PG 1SDR AWXA200100461Bulkhead · crackedMCN - C21 CK - C - BS 178 PRESS BULKHEAD CENTER WEB HAS A .5 INCH CRACK, WL 234, LBL 10 AT A FASTENER HOLE AS DETERMINED WITH HFEC. MAINTENANCE CUT OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED REPAIR PARTS IAW AWA ER 15-5312-01249-DSDR AWXA200100462Bulkhead · crackedMCN - C21 CK - C - BS 178 PRESS BULKHEAD CENTER WEB, AFT SIDE HAS A 1 INCH CRACK, LBL .7, WL 185 FOUND VISUALLY AND CONFIRMED WITH HFEC. MAINTENANCE CUT OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED REPAIR PARTS IAW B737 SRM 53-10-11SDR AWXA200100453Shear Tie · corrodedMCN - C-21 CK - "C" - FUSELAGE SKIN BULGE AND CUPPED FASTENERS IN SKIN AT BS 977, BETWEEN STR 23R TO 24R. MAINTENANCE REMOVER FASTENERS IN SKIN, NO CORROSION FOUND ON FUSELAGE SKIN, HOWEVER FOUND SHEAR TIE CORRODED BS 965, RBL 20. REMOVED AND REPLACED SHEAR TISDR AWXA0002158Keelbeam · damagedOIL CANNING AND LOOSE RIVETS ON KEEL BEAM PANEL BS 663-673. REPAIRED FASTENER HOLES IN KEEL BEAM CHORD AND REPAIRED PANEL IAW AWA ER 15-5315-01215-DL.SDR AWXA0002157Angle · corrodedD: Corrosion on torque box outlet support (BS 1088 bulkhead)C: Removed and replaced BS 1088 outlet support angle IAW BAC DWG 65-46572 and B737 SRM 51-10-6 Pg 4-6, 53-10-1 fig 8n Pg 4-5, 51-10-2 pg 7-8, 51-30-5 pg 5 and 51-30-2 pg 32SDR AWXA0002155Floorbeam · corrodedCORROSION ON FLOORBEAM BS 1016 LBL 33.5 TOP AND BOTTOM OF UPPER FLANGE. REPAIRED BS 1016 FLOORBEAM UPPER CHORD IAW AWA ER 15-5365-01209-DD1.SDR AWXA0002078Keelbeam · crackedOIL CANNING AND LOOSE RIVETS ON KEEL BEAM PANEL BS 663-673. REPAIRED FASTENER HOLES IN KEEL BEAM CHORD AND REPAIRED PANEL IAW AWA ER 155315-01215-DL3.SDR AWXA0002153Angle · crackedCABIN FLOORBEAM AREA ANGLE CRACKED BS 663.75 RBL 24. REPAIRED BS 663.75 BEAM UPPER CHORD IAW AWA ER 15-5715-01195-SS2.SDR AWXA0002152Spar · gougedD: LH horizontal stabilizer I/B upper attach lug at rear spar has 2 gouges.C: Repaired LH horizontal stabilizer rear spar upper attach lug IAW AWA ER 15-5510-01204-DD2SDR AWXA0002151Beam · crackedD: BS 706-717 BL.07 transverse floor beam cracked 8 EA PlacesC: Repaired beam IAW AWA ER 15-5702-01209-DD2SDR AWXA0002149Web · crackedD: 5 Cracks inweb below BL 24L Seat track BS 705-720C: Repaired web IAW ER 15-5715-01200-DL4SDR AWXA0002148Stringer · corrodedD: 2 SQ IN. corrosion found on stringer 26LT at BS 375C: Repaired stringer 26LT at BS 375 IAW B737 SRM 53-10-3 Fig 1 Pgs 1-10SDR AWXA0002100Web · crackedD: S-18A R/H shear beam web cracked.C: Replaced web 65-46877-82 per DWG 65-46877 - 76 INST. IAW SRM 51-10-1 page 8,9,10SDR AWXA0002096Floorbeam · crackedCABIN FLOORBEAM AREA ANGLE CRACKED BS 663.75 RBL 24. REPAIRED BS 663 BEAM UPPER CHORD IAW AWA ER 15-5715-01195-SS2.SDR AWXA0002076Spar · gougedD: LH Horizontal stabilizer I/B upper attach lug at rear spar has 2 gougesC: repaired LH horizontal stabilizer rear spar upper attach lug IAW er 15-5510-1204-DD2SDR AWXA0002073Web · crackedD: 5 Cracks in web below BL24L seat track BS 705-720C: Repaired web IAW AWA ER 15-5715-01200-DL4SDR AWXA0002072Hydraulic Line · looseHYDRAULIC PRESSURE LINE AT TRANSITION THROUGH PYLON, LOOSE, NR 1 PYLON. REPAIRED NR 1 HYDRAULIC PRESSURE LINE WALL PYLON IAW AWA ER 15-5412-01202-DL1.SDR AWXA0002101Floor Support · corrodedAFT CABIN - CORROSION ON FLOOR SUPPORT BEAMS BETWEEN STN 1000-1010 LBL 45. REPLACED BOTH FLOOR SUPPORT PER DRAW 65-46812 PART NUMBER 65-46812-87 AND 65-46812-91 IAW SRM 51-10-1 PAGE 8, 9, 10.SDR AWXA0002099Seat · corrodedD: Aft cabin R/H track F.STN.1006-1016 RBL 45 corroded.C: R/H floor track F.STN.1006-1016 RBL 45 DRAW 65C80735 - part no. 65C80735-115 and IAW SRM 51-10-1 Page 8,9,10SDR AWXA0002094SkinD: Fuselage R/H Skin STA 727-777 STR 14R-20R found to have several existing skin repairs adjacent to each other.C: repaired per ER 15-5331-01206-SS3SDR AWXA0002093Door Frame · crackedFWD ENTRY DOOR AFT FRAME AND INNER WEB CRACKED. REPAIRED DOOR AFT FRAME AS PER SRM 51-40-3 PG 1-6. REPAIRED DOOR WEB AS PER SRM 51-40-2 PG 1-3.SDR AWXA0002146Frame · crackedBS 663.75 PRESSURE DECK COMPRESSION CHORD CRACKED AT LBL 24. REPAIRED COMPRESSION CHORD IAW ER 15-5715-01195-SS2.SDR AWXA0002145Stringer · corrodedD: Bulge in skin with cupped fastener heads approx BS 360 STR 28 LTC: Repaired corrosion on lower tee chord and skin at BS 360 STR 28 LT IAW AWA ER 15-5314-01212-DL1SDR AWXA0002090Skin · corrodedLIGHT CORROSION ON SURFACE FOUND UNDERNEATH VHF ANTENNA COVER AT BS 777 & BL 0. CORROSION REMOVED PER SRM 53-30-1 FIG 1 PG 1. MADE AND INSTALLED NEW ANGLES PER DWG 65-49917 P/N 65-49917-11 AND 65-49917-12. INSTALLED NEW DOUBLERS AND FILLER PER SRM 53-30-3 FSDR AWXA0002070Frame · crackedBS 663.75 PRESSURE DECK COMPRESSION CHORD CRACKED AT LBL 24. REPAIRED COMPRESSION CHORD IAW AWA ER 15-5715-01195-SS2.SDR AWXA0002144Channel · crackedD: BS 665 LBL 24 upper chord cracked.C: Stop drilled and repaired BS 665 LBL 24 WL 207 chord crack IAW AWA ER 155702-01211-JS1SDR AWXA0002143Web · crackedD: BS 178 bulkhead web cracked 3 places at WL 189 between RBL .6 and LBL .6C: Repaired BS 178 bulkhead web IAW AWA E.R. 15-5312-01194-SS1SDR AWXA0002069Channel · crackedD: BS 665 LBL 24 upper chord Cracked.C: Stop drilled and repaired BS 665 LBL 24 WL 207 chord crack IAW AWA ER 15-5702-01211-JS1SDR AWXA0002054Web · crackedD: BS 178 Bulkhead Web cracked 3 places at WL 189 between RBL .6 and LBL .6C: Repaired BS 178 Bulkhead web IAW E.R. 15-5312-01194-SS1SDR AWXA0002092Bulkhead · crackedNDT FOUND CRACKS AT BS 178 WL 222 LBL 3 AND BS 178 WL 222 RBL 3. DAMAGED REPAIRED PER ER 15-5313-01212-DD1.SDR AWXA0002137Stiffener · corrodedD: Web support beam at R/H APU torque box BS 1098 has exfoliated corrosion on stiffenerC: Repaired web support beam stiffener IAW B737 SRM 51-40-3 Fig 1 pgs 1-6 and BAC DWG 65-54-832SDR AWXA0002050Stiffener · corrodedD: Web support beam at R/H APU torque box BS 1098 has exfoliated corrosion on stiffener.C: Repaired web support beam stiffener IAW B737 SRM 51-40-3 Fig 1 Pgs. 1-6 and BAC DWG 65-54832SDR AWXA0002136Stiffener · crackedD: Pressure web stiffener cracked at BS 727, LBL 17, WL 202C: Removed and replaced stiffener IAW B737 SRM 51-30-2 pg 8SDR AWXA0002135Stringer · corrodedD: Corrosion on STR 25R at BS 907 String Splice.C: Removed String & String Splice and attach angles, replaced string and splices and attach parts, fabed splices and string IAW B737 SRM 53-10-3SDR AWXA0002088Seat TrackD: Seat track @ RBL 24-75 STA 360-947 Nicked at Various Locations.C: Track blended at various locations and Assessed Per SRM 53-10-1 Pg 18. Track repaired per SRM 51-30-2 PG 8, SRM 53-10-5 pg 2, SRM 53-10-1 pg 8, SRM 53-10-5 PG 8SDR AWXA0002089Skin · crackedD: Aft service doorway Fwd Lwr corner cutout is cracked.C: Crack repaired as per SRM 53-30-3 Fig 24 pg 83-86H
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