Boeing 737-7Q8
Service difficulty reports · 3,961
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 = '7377Q8' 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 = '7377Q8' 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 SWAA2026012964966Smoke Detector · false activationFWD LAVATORY SMOKE DETECTOR ACTIVATED IN CLIMB & DESCENT. RESET BOTH TIMES. NO EVIDENE OF SMOKE OR ODOR. OK TO CONT PER MEL 26-16-01, SP1B, AND SP3. R & R THE SMOKE DETECTOR IAW AMM 26-14-01, OPS CHECKED GOOD.SDR SWAA2026012162844Battery Pack · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M2335 INOPERATIVE. REPLACED THE BATTERY PACK M2335 IAW AMM 33-51-06-960-805. OPS CHECKED GOOD IAW AMM 33-51-06-960-805.SDR SWAA2026012062157Seat Back · loosePASSENGER SEAT ROWS 11 DEF, SEAT BACK LOOSE. TIGHTENED THE SEAT BACK IAW CMM 25-21-45, REV 6, STEP 3.Y.(6).SDR SWAA2026012062162Seat Back · loosePASSENGER SEAT ROWS 11 BC, SEAT BACK LOOSE. TIGHTENED THE SEAT BACKS IAW CMM 25-21-45, REV.6, STEP 3.Y.SDR SWAA2026012062159Cover · out of adjustPAX CABIN AFT RT DOOR SLIDE LOWER COVER RUBBING AGAINST WITH THE DOOR SCUFF PLATE AT CLOSE POSITION. INSTALLED CORRECTLY PAX CABIN AFT RT DOOR SLIDE LOWER COVER IAW AMM-25-66-01-000-802, AND MT 725-61-06.SDR SWAA2026012062150Assist Handle · loosePAX CABIN FWD ENTRY DOOR ASSIST HANDLE LOOSE. TIGHTENED PAX CABIN FWD ENTRY DOOR ASSISTANT HANDLE IAW AMM 52-11-31-400-802, STEP 3 G(2).SDR SWAA2026011962155Fitting · looseAFT GALLEY L2 DOOR AFT GIRT BAR FITTING LOOSE. TIGHTENED AFT GALLEY L2 DOOR AFT GIRT BAR FITTING IAW AMM-25-66-02-400-801. TESTED OK.SDR SWAA2026012161745Battery Pack · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1674 INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK M1674 AND TESTED GOOD IAW AMM 33-51-06-960-805.SDR SWAA2026012161746Battery Pack · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1668 INOPERATIVE. REMOVED AND REPLACED BATTERY PACK M1668 AND TESTED GOOD IAW AMM 33-51-06-960-805.SDR SWAA2026012258782Frame · crackedCRACKED FRAME, BS 787, S8L. REPAIRED THE FRAME IAW EA 1-A53-12114, REV B.SDR SWAA2026012657849Seat Track · corrodedPASSENGER CABIN SEAT TRACK CORRODED, RBL 25, BS 380 ON CROWN & WELL, BS 380+14 IN WELL, BS 400+4 IN WELL, BS 400+14 IN WELL, BS 420+4 ON CROWN, BS 440+2 IN WELL, BS 440+13 IN WELL, WL 208. SRM 53-00-52-1A-1 IS APPLICABLE ALLOWABLE DAMAGE. REMOVED CORROSISDR SWAA2026012657685Plate · crackedCRACKED WIGGLE PLATE ASSY, IRSS 199+13, LT WING REAR SPAR. REMOVED THE WIGGLE PLATE IAW SRM 51-40-02-0G-0. RECEIVED A NEW WIGGLE PLATE, AND INSTALLED IAW SRM 51-40-02-0G-0.SDR SWAA2026012257195Scuff Plate · crackedAFT CARGO BAY AFT CORNER SCUFF PLATE CRACKED. REPAIRED THE SCUFF PLATE IAW SRM 53-60-15-2R-1.SDR SWAA2026012257194Handle · looseAFT SERVICE DOOR LOOSE ASSIST HANDLE. REMOVED AND REINSTALLED AFT SERVICE DOOR ASSIST HANDLE IAW AMM 52-41-31-000-802 STEP 2. E. (4). AND AMM 52-41-31-400-802 STEP 3. F.(2).SDR SWAA2026012157218Fitting · looseAFT ENTRY DOOR AFT GIRT BAR FITTING LOOSE. TIGHTENED AFT ENTRY DOOR AFT GIRT BAR FITTING LOOSE IAW SOPM 20-50-02 & SOPM 20-50-01.SDR SWAA2026012157223Fitting · looseAFT ENTRY DOOR SLIDE AFT GIRT BAR FITTING LOOSE. REMOVED AND INSTALLED AFT ENTRY DOOR SLIDE AFT GIRT BAR FITTING IAW SRM 51-40-02-0G, STEPS 2. B.SDR SWAA2026012657079Skin · crackedONE CRACK NOTED ON THE LT HORIZONTAL STAB LOWER SKIN HSS 193.90, 18 INCHES FROM THE FWD EDGE, L: 0.4'. REPAIRED THE LT LOWER HORIZONTAL STAB SKIN IAW SRM 55-10-01-2R-11.SDR SWAA2026012357171Duct · crackedE/E BAY COOLING EXHAUST DUCT AFT FLANGE IS CRACKED. THE DUCT WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. REMOVED AND INSTALLED NEW COOLING EXHAUST DUCT IAW AMM 21-27-10.SDR SWAA2026012357176Floor Panel · delaminatedFLOOR PANEL 242DF AFT CORNERS ARE DELAMINATED. FABRICATION OF NEW 242DF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.SDR SWAA2026012257077Pressure Deck · crackedCRACK FOUND ON THE HORIZONTAL PRESSURE DECK IN THE MID CABIN, BS 663+2, LBL 32, L 0.35". REMOVED THE DAMAGE PART OF THE HORIZONTAL PRESSURE DECK BS 663 - 674, LBL 30 - 60, WL 202, AND REPAIRED IAW SRM 53-40-51-2R-2, REPAIR 2.SDR SWAA2026012257185Attach Angle · crackedBS 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE CRACKED, RBL 10, WL 167. REMOVED THE DAMAGED SECTION OF THE ANGLE AND INSTALLED IAW DWG 111A1000, REV -, &SRM 57-10-10-2R-5, REPAIR 5.SDR SWAA2026012257072Floor Panel · debondedFLOOR PANEL 193B DEBONDED ON INNER SURFACE. REPAIRED THE FLOOR PANEL IAW SRM 51-70-05-2R-2-A00733, REPAIR 2.SDR SWAA2026012257078Skin · crackedCRACK AROUND THE FASTENER AT NR 7 SLAT LOWER SURFACE OF THE L/E SLAT NOSE SKIN AT ACTUATOR RIBS. REPAIRED NO.7 SLAT LOWER SURFACE OF THE L/E SLAT NOSE SKIN AT ACTUATOR RIBS IAW SRM 57-42-01-2R-8.SDR SWAA2026012257173Floor Panel · delaminatedFLOOR PANEL 231YF IS DELAMINATED ON UPPER SURFACE. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF DAMAGE IAW SRM 53-00-50-2R-0, DWG 144A5810.SDR SWAA2026012257172Floor Panel · delaminatedFLOOR PANEL 231ZF IS DELAMINATED ON UPPER SURFACE. FABRICATED A NEW 231ZF FLOOR PANEL REPLACEMENT. ACCOMPLISHED IAW SRM 53-00-50-2R-0.SDR SWAA2026012257174Floor Panel · delaminatedFLOOR PANEL 232RF AFT END IS DELAMINATED. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF DAMAGE IAW SRM 53-00-50-2R-0, DWG 144A5810.SDR SWAA2026012257175Floor Panel · delaminatedFLOOR PANEL 241BF IS DELAMINATED ON UPPER SURFACE. THE FLOOR SUPPORT WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF DAMAGE IAW SRM 53-00-50-2R-0, DWG 144A5810.SDR SWAA2026012257179Floor Panel · delaminatedFLOOR PANEL 241CF AFT CORNERS ARE DELAMINATED. THE FLOOR PANEL 241CF REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF DAMAGE IAW SRM 53-00-50-2R-0, DWG 144A5810.SDR SWAA2026012257180Floor Panel · delaminatedFLOOR PANEL 242AF IS DELAMINATED ON UPPER SURFACE. REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0, DWG 144A5810.SDR SWAA2026012257181Floor Panel · delaminatedFLOOR PANEL 241EF AFT CORNERS ARE DELAMINATED. REPLACED WITH A NEWLY FABRICATED FLOOR PANEL; DUE TO THE EXTENT OF ALL OF THE DAMAGE IAW SRM 53-00-50-2R-0 AND DRAWING 144A5810-129.SDR SWAA2026012257182Floor Panel · delaminatedFLOOR PANEL 242CF AFT CORNERS ARE DELAMINATED. FABRICATION OF NEW 242CF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.SDR SWAA2026012056564Fitting · crackedCRACKED FITTING LOCATE FRONT SPAR INSPAR RIB HSS 120.30 RT HORIZONTAL STABILIZER. REPLACED FITTING LOCATE FRONT SPAR INSPAR RIB HSS 120.30 RT HORIZONTAL STABILIZER IAW EA 26-155-00100-WIP1.SDR SWAA2026012056563Rib · crackedCRACK INSPAR RIB LOC FWD UPPER CHORD STAB 120.30 AND 1IN FROM FRONT SPAR HSS 120.30 AT RT HORIZONTAL STAB. REPAIRED INSPAR RIB LOC FWD UPPER CHORD STAB 120.30 AND 1IN FROM FRONT SPAR STAB 120.30 AT RT HORIZONTAL STAB IAW EA 26-155-00100-WIP1.SDR SWAA2026012056565Rib · crackedCRACK IN SPAR RIB LOCATED FWD LOWER CHORD STAB 120.30 AND 1 INCH FROM FRONT HSS 120.30 AT RT HORIZONTAL STAB. REPAIRED INSPAR RIB LOC FWD LOWER CHORD HSS 120.30 AND 1IN FROM FRONT SPAR STAB 120.30 AT RT HORIZONTAL STAB IAW EA 26-155-00100-WIP1.SDR SWAA2026012056575Plate · crackedCRACK ON CORRUGATED PLATE LOCATED TRAILING EDGE ORSS261 AT RT WING. REPLACED CORRUGATED PLATE AND FASTENERS LOCATED TRAILING EDGE ORSS261 AT RT WING IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 115A2001, SHEET 29, REV-.SDR SWAA2026012056583Plate · crackedCRACK ON CORRUGATED PLATE LOCATED TRAILING EDGE IRSS216 AT LT WING. REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE IRSS216 AT LT WING IAW SRM 51-0-02, ITEM 9, SRM 51-40-02, AND DWG 115A2001, SHEET 29, REV- .SDR SWAA2026012056587Plate · crackedCRACK ON CORRUGATED PLATE LOCATED TRAILING EDGE ORSS261 AT LT WING. REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE ORSS261 AT LT WING IAW SRM 51-0-02, ITEM 9, SRM 51-40-02 AND DWG 115A2001, SHEET 29, REV- .SDR SWAA2026012056580Plate · crackedCRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS241 AT RT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS241 AT RT WING IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 115A2001, SHEET 30, REV A.SDR SWAA2026012056582Support Bracket · crackedCRACK ON SUPPORT BRACKET TRAILING EDGE LOCATED ORSS273 RT WING. REPLACED SUPPORT BRACKET AND FASTENERS LOCATED ON TRAILING EDGE ORSS273 RT WING. MEASUREMENT OF CRACK IS: L=0.927.SDR SWAA2026012056586Plate · crackedCRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS241 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS241 AT LT WING IAW SRM 51-10-02, ITEM 9, SRM 51-40-02 AND DWG 115A2001, SHEET 30, REV A.SDR SWAA2026012056588Support Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED TRAILING EDGE ORSS273 INTERNAL AREA AT LT WING. REPLACED SUPPORT BRACKET LOCATED TRAILING EDGE ORSS273 INTERNAL AREA AT LT WING. MEASUREMENT OF CRACK IS: L=0.653.SDR SWAA2026012056584Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED TRAILING EDGE ORSS273 AT LT WING. REPLACED SUPPORT ANGLE LOCATED TRAILING EDGE ORSS273 AT LT WING IAW SRM 51-10-02, ITEM 9; SRM 51-40-02 AND DWG 115A2930 SHEET 6 REV -. MEASUREMENT OF CRACK IS: L= 2.437.SDR SWAA2026011956589Beam · crackedCRACKED BEAM LOCATED TRAILING EDGE ORSS285 AT LT WING. REPLACED BEAM AND FASTENERS LOCATED TRAILING EDGE ORSS285 AT LT WING IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 115A3700; SHEET 31, REV -, AND DRAWING 115A3712, SHEET 5, REV -.SDR SWAA2026011955971Rib · crackedCRACKED INSPAR RIB 120.30 LOCATED AT 36 INCHES OF FRONT SPAR AT RT HORIZONTAL STAB. REPAIRED INSPAR RIB LOCATED STAB STA 120.30 AND 36 INCH FROM REAR SPAR AT RT HORIZONTAL STABILIZER IAW SRM 55-10-09-2R-5, REPAIR 5.SDR SWAA2026012055861Access Panel · damagedELONGATED HOLE ON ACCESS PANEL 571EB TRAILING EDGE AT LT WING. REPAIRED ACCESS PANEL 571EB TRAILING EDGE AT LT WING IAW SRM 51-70-04-2R-9 REPAIR 9. STEP 14 BASED ON THE REPAIR PERFORMED IS TO SECONDARY STRUCTURE. IAW MPM 10.3.4 RII IS ONLY REQUIRED FOR MAJORSDR SWAA2026011955860Scuff Plate · crackedCRACKED AFT CORNER SCUFF PLATE AT AFT CARGO BAY. REPAIRED AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, PARAGRAPH 4. B; STEPS 2 AND 4 TO 7.SDR SWAA2026011955701Plate · crackedCRACKED CORRUGATED PLATE TRAILING EDGE IRSS 215 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE IRSS 215 AT LT WING IAW SRM 51-40-02; SRM 51-10-02 ITEM 9; DWG 115A2001 SHEET 30 REV A AND DWG 115A2713 SHEET 3 REV A.SDR SWAA2026011955702Support Bracket · crackedCRACK TRAILING EDGE FIXED PANEL SUPPORT BRACKET AT LEVEL ORSS 271 AT LT WING. REPLACED SUPPORT BRACKET LOC. TRAILING EDGE FIXED PANEL AT LEVEL ORSS 271 AT LT WING IAW SRM 51-40-02-0G-0 AND SRM 51-10-02-0G-0 ITEM 9. MEASURE OF CRACK IS: L: 0.646 INCHES.SDR SWAA2026011555699Plate · noneCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 241 AT LT WING. PERFORMED VISUAL INSPECTION ON CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 241 AT LT WING AND NOT FOUND CRACK PAINT MARKET ONLY; PERFORMED CLEAN IAW SRM 51-10-04.SDR SWAA2026011555700Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE ORSS 261 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE, ORSS 261 LT WING IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, & DWG 115A2001, SHEET 29, REV-.
Back to Boeing 737-7Q8