Boeing 737-7H4
Service difficulty reports · 96,125
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 = '7377H4' 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 = '7377H4' 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 SWAA2026091100219Scuff Plate · crackedCRACK ON AFT CORNER SCUFF PLATE IN THE AFT CARGO BAY. REPAIRED THE AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, PARAGRAPH 4. B, STEPS (2 TO 7) FIGURE 203.SDR SWAA2026091164233Skin · crackedCRACK INDICATION FOUND ON HORIZONTAL STAB LOWER SKIN, RT SIDE. HSS 193.90, RIB INBD SIDE & 16.5 INCH FRONT SPAR TO REAR SPAR. CRACK LENGTH 0.563 INCH. REPAIRED THE HORIZONTAL STAB LOWER SKIN PANEL. LOCATED BTW STAB STA 184.70 AND STAB STA 203.10 AT RT HORIZOSDR SWAA2026090819205Crossbeam · crackedCRACKED CROSSBEAM, BS 540, LBL 24.75 - 45.5, WL 208.1. REPLACED THE CROSSBEAM & FASTENERS IAW SRM 51-40-02, & DWG 143A0060, SHEET 36, REV A.SDR SWAA2026090879801Lens · brokenBROKEN EMERGENCY LIGHT LENS. REPLACED THE EMERGENCY LIGHT LENS IAW AMM 33-51-01-960-801, STEP 2.C.(1)(A) 4), AND 2.C.(4).SDR SWAA2026090836589Crossbeam · crackedCRACKED CROSSBEAM, BS 540, LBL 45.50 - 60, WL 208.1. REPLACED THE CROSSBEAM IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, STEP 9, AND DWG 143A5240, SHEET 21, REV- .SDR SWAA2026090753324Rib · crackedLEFT HORIZONTAL STAB RIB NR 4, 2ND STIFFENER FROM FWD, CRACKED. RIB REPAIRED IAW SRM 55-10-09-2R-4-A01101.SDR SWAA2026082421076Hook · brokenCREW REPORTS FWD ENTRY DOOR GRIT BAR STOW HOOK BROKEN RIVET ON FWD HOOK. ACCOMPLISHED REPAIR PER EA M-23-125-01839 OPTION 1 TEMP REPAIR, OK TO CONTINUE IAW EA.SDR SWAA2026082421958Light · inoperativeAFT ENTRY EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED IAW AMM 33-51-01-960-801.SDR SWAA2026082483248Flashlight · inoperativeFLT ATTENDANT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FWD F/A FLASHLIGHT IAW AMM 25-64-00. OPS CHECKED GOODSDR SWAA2026092313059Nut Plate · crackedCRACKED NUT PLATE, OFSS 604, INTERNAL CAVITY LEADING EDGE, RT WING. REPLACED THE NUT PLATE BTWN OSS 362.51 - 384.24. IAW SRM 51-40-02, & DWG 112A4402, SHEET 14, REV-.SDR SWAA2026092332053Doubler · damagedELONGATE HOLE ON DOUBLER ON REAR SPAR, RT VAPOR BARRIER BS 663 BTWN RBL12 - 27. FABRICATED A DOUBLER, & LOCATED IAW DWG 111A1512, SHT 3, REV-.SDR SWAA2026092106314Nut Plate · crackedCRACKED NUT PLATE, OFSS 404, INTERNAL CAVITY L/E OF LT WING. REPLACED THE NUT PLATE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 112A4402, SHEET 40, REV A.SDR SWAA2026092101997Support Frame · damagedELONGATE HOLE ON FRAME ON RT VAPOR BARRIER BTWN BS 655 - BS 693, RBL 12. EVALUATED & FABRICATED THE FRAME IAW SRM 51-40-05-0G-0, & DWG 149A7214, SHEET 7, REV -. DOUBLER INSTALLATION WILL BE ACCOMPLISHED TTG8Q01DQJAS.SDR SWAA2026092127237Nut Plate · crackedCRACKED RAIL NUT PLATE LOC OFSS 570, INTERNAL CAVITY LEADING EDGE OF RT WING. REMOVED THE NUT PLATE IAW SRM 51-40-01 AND PERFORMED VISUAL INSPECTION ON ADJACENT AREAS AND DID NOT FIND OTHER DAMAGE. REPLACED THE NUT PLATE IAW SRM 51-40-01, SRM 51-40-02, SRM SDR SWAA2026092139892Strap · crackedCRACK INDICATION ON STA 639 AT LBL 45.57 STUB BEAM STRAPS AREA (IN AFT FASTENER HOLE) AT PASSENGER CABIN. REPLACED STRAPS (2EA) LOCATED AT STUB BEAM BTW STA 639 AT LBL 45.57 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 DWG 144A1705 SHEET:8 REV:- AND DWSDR SWAA2026092130117Nut Plate · crackedCRACKED RAIL NUT PLATE, OFSS 491 INTERNAL CAVITY LEADING EDGE IN THE RT WING. REPLACED RAIL NUT PLATE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 112A4402, SHEET 40, REV A.SDR SWAA2026092188030Nut Plate · crackedCRACKED RAIL NUT PLATE, OFSS 385 INTERNAL CAVITY LEADING EDGE OF THE LT WING. REPLACED THE RAIL NUT PLATE IAW SRM 51-40-02, AND DWG 112A4402, SHEET 40, REV A.SDR SWAA2026092147620Nut Plate · crackedCRACKED RAIL NUT PLATE, OFSS 337 INTERNAL CAVITY LEADING EDGE OF LT WING. REPLACED THE NUT PLATE IAW SRM 51-40-02, AND DWG 112A4402, SHEET 40, REV A.SDR SWAA2026092127663Nut Plate · crackedCRACKED RAIL NUT PLATE, OFSS 588 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT PLATE IAW SRM 51-40-02-0G-0, & DWG 112A4402, SHEET 13, REV-.SDR SWAA2026092109501Nut Plate · crackedCRACK RAIL NUT PLATE LOC OFSS 449 INTERNAL CAVITY LEADING EDGE AT RT WING. REPLACED THE NUT PLATE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG:112A4402, SHEET 40, REV A.SDR SWAA2026092186645Nut Plate · crackedCRACKED RAIL NUT PLATE LOC OFSS 491 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT PLATE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 112A4402, SHEET 40, REV A.SDR SWAA2026091814040Support Angle · crackedCRACKED CARGO LINER SUPPORT ANGLE, BS 727B, LBL 51 IN THE AFT CARGO BAY. REPLACED THE SUPPORT ANGLE BTWN BS 727A - 727E+10 IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, & DWG 149A9490, SHEET 21, REV -.SDR SWAA2026091837580Support Angle · crackedCRACK CARGO LINER SUPPORT ANGLE LOC STA 727C LBL 51 AT AFT CARGO BAY. REPLACED CARGO LINER SUPPORT ANGLE LOCATED BTW BS727A TO BS727E+10 AT AFT CARGO COMPARTMENT IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 149A9490, SHEET 21, REV -.SDR SWAA2026091883552Support Angle · crackedCRACKED CARGO LINER SUPPORT ANGLE, BS 727E, LBL 51 IN THE CARGO BAY. REPLACED THE SUPPORT ANGLE BS 727A - 727E+10 IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 149A9490, SHEET 21, REV -.SDR SWAA2026091802628Crossbeam · crackedCRACKED BRAKE PANEL LOCATED BS 540 BTW RBL 24.75 TO RBL 45.5 WL 208.1 AT PASSENGER CABIN. REPLACED BRAKE PANEL LOCATED BS 540 BTW RBL 24.75 TO RBL 45.5 WL 208.1 AT PASSENGER CABIN IAWSRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG: 143A0060 SHEET: 46 REV: -SDR SWAA2026091864779Crossbeam · crackedCRACK ON BRAKE PANEL LOCATED BS 540 BTW LBL 24.75 TO LBL 45.5 WL 208.1 AT PASSENGER CABIN. REPLACED BRAKE PANEL IAW SRM 51-10-02 ITEM 9 AND DWG 143A0060, SHEET 46, REV -.SDR SWAA2026091815453Crossbeam · crackedCRACK ON BRAKE PANEL LOCATED BS 540 BTW BL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABIN 2026-490319 REPLACED BRAKE PANEL LOCATED BS 540 BTW BL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABIN I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG: 143A0060 SHEETSDR SWAA2026090856707Scuff Plate · crackedCRACKED SCUFF PLATE ON FWD SERVICE DOOR. REPAIRED SCUFF PLATE ON FWD SERVICE DOOR AT FWD GALLEY AREA IAW SRM 53-10-15-2R-2, REPAIR 2.SDR SWAA2026090813201Rib · crackedCRACK FOUND ON RT OTBD AFT FLAP INBD RIB 4TH HOLE APPROX. .060". RT OTBD AFT FLAP WAS REPLACED WITH A SERVICEABLE FLAP ON CARD TTG8Q01BR3TM.,SDR SWAA2026090875897Strap · crackedR/H STA 639 STUB BEAM STRAP CRACK INDICATION FOUND IN AFT HOLE. REMOVED AND REPLACED STUB BEAM STRAP AT BS 639 RBL 45 IAW SRM 51-40-02-0G-0 DWG BOEING 144A1715 REV A AND 144A1505 REV - .SDR SWAA2026082502929Seal · pinchedDIVERSION FOR SQUEALING IN THE HEADSETS. PERFORMED EXTERNAL LEAK CHECK OF FLIGHT DECK WINDOWS PER AMM 055191. LOUD SQUEAL FROM F\O NR 2 WINDOW FWD EDGE NOTED FROM INSIDE ONLY AND VERY LOUD. REMOVED OBSTRUCTION FROM WINDOW FWD EDGE SEAL. REPEATED TEST IAW AMMSDR SWAA2026082449316Battery Pack · inoperativeMAIN CABIN MULTIPLE EMERGENCY LIGHTS INOPERATIVE. R & R THE BATTERY PACK M1673 & PERFORMED SATISFACTORY OPS CHECK IAW AMM 33-51-06.SDR SWAA2026082139058Handle · brokenCAPTAINS GRAB HAMDLE BROKEN. R & R HANDLE IAW SIP. NO DEFECTS NOTED.SDR SWAA2026082066279Engine · failedNR 1 ENG, LOUD BANG DURING CLIMB OUT. REMOVED AND REPLACED NR 1 ENGINE IAW MT 771-00-01 ON TTG8Q006VJKP.SDR SWAA2026092309524Support · scratchedSCRIBE MARKS LOCATED ON SUPPORT ZEE BTW BS 400 - 488, LBL 21.8, IN THE FWD CARGO BAY. PERFORMED A PERMANENT REPAIR ON THE SUPPORT ZEE IAW SRM 53-00-53-2R-6, REPAIR 6.SDR SWAA2026092374341Bracket · damagedELONGATE HOLE ON BRACKET ASSY LOCATED AT RT VAPOR BARRIER BS 663, RBL 31. EVALUATED & FABRICATED BRACKET ASSY IAW SRM 51-40-05-0G-0, & DWG 287A9112, SHEET 13, REV. A. FOR INSTALLATION OF THE BRACKET, SEE TTG8Q01DQJA.SDR SWAA2026092192990Strap · missingMISSING STRAP ON LIFE LINE OF THE EMERGENCY DOORS LT & RT. INSTALLED THE STRAP ON LIFE LINE IAW SOPM 20-50-12, REV 56, & DWG 416A1500, REV-.SDR SWAA2026092135422Web · crackedCRACKED WEB LOCATED BTWN BS 500D - 520, STR 28L IN THE FWD CARGO BAY. REPLACED THE WEB AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7902, SHEET 126, REV A.SDR SWAA2026082178201Handle · loosePAX CABIN FWD ENTRY DOOR LOWER ASSIST HANDLE LOOSE. INSTALLED THE ASSIST HANDLE CORRECTLY IAW AMM 52-11-31-400-802 STEP 3.G.(2).SDR SWAA2026082035044Fuse · inoperativeCREW REPORTS RH OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOPERATIVE. OK TO CONTINUE ON MEL 33-2-03 SP1B AUTH# 334898. R & R RT OVERWING DOOR LIGHT FUSE IAW AMM 33-51-06, OPS CHKD GOOD.SDR SWAA2026082038923Lamp · inoperativeAREA EMERGENCY LIGHT AT SEAT 8ABC INOPERATIVE. REPLACED THE LAMPS, OPS TESTED GOOD IAW AMM 33-51-03-960-801.SDR SWAA2026082063813Slide · out of positionFORWARD GALLEY SERVICE DOOR SLIDE DRAGS EXCESSIVELY WHEN OPENING DOOR. REPOSITIONED EXISTING SLIDE SO IT WOULD NOT DRAG WHEN OPENED PER 725-61-06-FSSDR SWAA2026081816132Flap System · lockedFLAPS LOCKED OUT AT POSITION 10. RIGHT NEEDLE INDICATED 12 DEGREES & LEFT NEEDLE INDICATED 11 DEGRESS. R+R T/E FLAP POSITION TRANSMITTER REF MM. 27-58-01 AND T/E FLAP INDICATOR REF MM 25-58-02 OPS CHECK GOOD.SDR SWAA2026092387797Support · damagedSCRIBE MARKS ON SUPPORT ZEE BTWN BS 727 - 847, LBL 21.80. REPLACED THE SUPPORT ZEE IAW SRM 51-40-02, AND DWG 146A7500, SHT 85, REV A.SDR SWAA2026092397570Elec Connector · damagedCUT ON GALLEY 1 EMERGENCY EXIT LIGHT CABLE. REPLACED THE CONNECTOR ON WIRE W4142 D03658 IAW SWPM 20-30-12, AND PERFORMED EMERGENCY LIGHT OPS TEST IAW AMM 33-51-00-710-801.SDR SWAA2026092376151Shield · corrodedCORRODED SHIELD WEB, BS 767 - 794.3, WL156, RBL 22. DRILLED DIAMETER FASTENERS HOLES (10 EA) TO ATTACH FLOOR PANEL TO SHIELD WEB. IAW SRM 51-40-05, & DWG 146A0081, SHT 46, REV -. DIAMETER HOLES IS 0.221 INCH.SDR SWAA2026092372218Gusset · crackedCRACKED GUSSET, BS 500D, S19L. REPLACED THE GUSSET AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7902, SHEET 174, REV -.SDR SWAA2026092345565Frame · dentedDENTED FRAME, BS 500B, STR 25L - 26L IN THE FWD CARGO BAY. MADE & DRILLED A REPAIR FOR FRAME BS 500B, STR 25L - 26L IAW SRM 53-30-07-2R-1, REPAIR 1, ALTERNATIVE 1.SDR SWAA2026092296142Lug · corrodedCORROSION ON REAR LOWER LUG AFT SIDE AT LT HORIZONTAL STAB. REPAIRED THE LUG IAW EA 26-155-02251-WIP1, EA 26-155-02251-WIP2, REV 2, EA 26-155-02251-WIP3, REV 2, EA 26-155-02251-WIP4, EA 26-155-02251-WIP5, & EA 26-155-02251.SDR SWAA2026092107956Hook · corrodedCORROSION ON LEFT EMERGENCY EXIT DOOR LIFE LINE HOOK. REPLACED THE LIFE LINE HOOK IAW AMM 25-61-10-000-802, AND AMM 25-61-10-400-802.
Back to Boeing 737-7H4