Boeing 737-76Q
Service difficulty reports · 1,627
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 = '73776Q' 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 = '73776Q' 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 SWAA2020041334088Spar · corroded**CORROSION*** EVIDENCE OF CORROSION AT RIGHT WING FRONT SPAR WEB AT IFSS 119 COMMON TO BOOST PUMP UPPER AND LOWER BONDING JUMPER FASTENER HOLES / REPAIRED R/W FRON SPAR WEB AT IFSS 119 COMMON TO BOOST PUMP UPPER AND LOWER BONDING JUMPER FASTENER HOLES IAW ATSSDR SWAA2020040933481Block · corrodedCORROSION ON FWD SEVICE DOOR BOTH FWD AND AFT GIRT BAR BLOCKS. / REMOVED BOTH FWD AND AFT GIRT BAR BLOCKS; FWD SERVICE DOOR AND REPLACED WITH NEW PER AMM 25-66-02-400-801SDR SWAA2020033033482Block · corrodedCORROSION ON AFT ENTRY DOOR BOTH FWD AND AFT GIRT BAR BLOCKS. / REMOVED AND INSTALLED NEW FWD AND AFT GIRT BAR BLOCKS AT AFT ENTRY DOOR AND PERFORMED INSTALLATION TEST; TEST GOOD PER AMM 25-66-02-000-801; 25-66-02-400-801.SDR SWAA2021072233341Floor Support · corroded(SKYLINE DTIP) PREVIOUS REPAIR AFT CARGO BAY FLOOR SUPPORT; STA 787-856; RBL 14; CORROSION REPAIRED / UPON FURTHER INVESTIGATION NO REPAIR AT NOTED LOCATIONSDR SWAA2021070783112Plate · pulledWIGGLE PLATE AT I/B SIDE OF RIGHT WING TRAILING EDGE PANEL (651GB) HAS PULLED FASTENER S / REMOVED AND REPLACED WIGGLE PLATE AT I/B SIDE OF RIGHT WING TRAILING EDGE PANEL 651GB; IAW SRM 51-40-02-0G-0. 84036U; 25MAR20.SDR SWAA2020032533019Floor Panel · damagedREPAIR TWO OPEN HOLES IN FLOOR PANEL 241ABF. / REPAIRED OPEN HOLES IN FLOOR PANEL 241ABF IAW SRM 53-00-50-2R-6SDR SWAA2021062432279Scuff Plate · crackedAFT CARGO BAY FWD CORNER SCUFF PLATE CRACKED / REPAIRED AFT CARGO BAY-FWD CORNER SCUFF PLATE PER EA #1-A53-2076 REV: 11.SDR SWAA2020041332277Skin · damagedFUSELAGE EXTERIOR SKIN REPAIR AT BS 302-310; STRINGER 17R-18R DOES NOT MEET SRM CRITERIA FOR FASTENER INSTALLATION AND ADEQUATE DAMAGE REMOVAL. / REMOVED FUSELAGE EXTERNAL SKIN REPAIR BS. 302-310 STR 17R/H-18R/H. REPAIRED PER ATS ER #20-02206 REV IR AND SWA EASDR SWAA2020040635640Structure · dentedFLIGHT DECK FLOOR IS DENTED AT B.S. 255; L.B.L. 14; W.L. 207.45 / ACCOMPLISHED FLIGHT DECK FLOOR REPAIR IAW EA 1-A53-33179SDR SWAA2020041331598Doubler · cracked(SKYLINE DTIP) FOUND PREVIOUS REPAIR ANGLE DOUBLER CRACKED; STA 294; ABOVE S-17R; LWR INBOARD FLANGE AT FASTENER HOLE. / REMOVED AND REPLACED STUB FRAME; STA 294; RBL 65 WL APPROX 230 TO 208. PER DWG 141A8370 AND SRM 54-40-02.SDR SWAA2020032508995Support · corroded***CORROSION*** ACB RH FLOOR-TO-SIDEWALL SUPPORT HAS MULTIPLE POINTS OF CORROSION; BS 727D TO 767; RBL 20; WL 156 / REMOVED AND REPLACED ACB RH FLOOR TO SIDEWALL SUPPORT B/S 727 TO 767; RBL 20; WL 156 IAW SRM 51-40-02 AND DWG 146A7500 REV:- 59899U; 17MAR20.SDR SWAA2020032442647Frame · cracked(SKYLINE DTIP) PREVIOUS REPAIR NOTED FUSELAGE FRAME, STA 294, ABOVE S-17R CRACK REPAIRED PER SRM 51-70-11-2R-1 FOUND PREVIOUS REPAIR DOUBLER CRACKED AT FRAME STA 294 ABOVE S-17R, PER SRM 51-70-11-2R-1, GENERATED NRC U154242 TO REPLACE REPAIR.SDR SWAA2021080508958Floor Panel · damagedAFT CABIN FLOOR PANEL 241XF HAS DAMAGED UPPER SURFACE SKIN / AFT CABIN FLOOR PANEL 241XF WITH DAMAGED UPPER SURFACE SKIN WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE PER SRM 51-10-02-0G-0 PARA 9.A.(1).SDR SWAA2021080508962Floor Panel · damagedAFT CABIN FLOOR PANEL 242UF HAS DAMAGED UPPER SURFACE SKIN / AFT CABIN FLOOR PANEL 242UF WITH DAMAGED UPPER SURFACE SKIN WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE PER SRM 51-10-02-0G-0; PARA 9.A.(1).SDR SWAA2021080508963Floor Panel · damagedAFT CABIN FLOOR PANEL 242WF HAS DAMAGED UPPER SURFACE SKIN / AFT CABIN FLOOR PANEL 242WF WITH DAMAGED UPPER SURFACE SKIN WAS REPLACED WITH A SERVICABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 51-10-02-0G-0 PARA 9.A.(1)SDR SWAA2021080508959Floor Panel · damagedAFT CABIN FLOOR PANEL 241AAF HAS DAMAGED UPPER SURFACE SKIN / AFT CABIN FLOOR PANEL 241AAF WITH DAMAGED UPPER SURFACE SKIN WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 51-10-02-0G-0 PARA 9.A.(1) 59812U 03/10/2020SDR SWAA2021080508960Floor Panel · damagedAFT CABIN FLOOR PANEL 241ABF HAS DAMAGED UPPER SURFACE SKIN / DAMAGED FLOOR PANEL 241ABF WAS REPLACED WITH A SERVICABLE PART IAW SRM 51-10-22-0G-0 PAR. 9SDR SWAA2020032508961Floor Panel · damagedAFT CABIN FLOOR PANEL 242VF HAS DAMAGED UPPER SURFACE SKIN / AFT CABIN FLOOR PANEL 242VF DAMAGED UPPER SURFACE SKIN WAS REPAIRED IAW SRM 53-00-50-2R-1. 56144U; 03/12/2020.SDR SWAA2020041336736Rudder · puncturedRUDDER L/H SIDE IS PUNCTURED 35' FROM BOTTOM / REPAIRED RUDDER L/H SIDE 35' FROM BOTTOM ON WORK ORDER #532072; FORM TRACKING #N137283. FUNCTIONAL TESTS PASSED. (POS: ONLY; TAGNO: 686535; P/N OFF/ON: 173A0103-8; S/N OFF: CASA-0069; S/N ON: CASA-0069)SDR SWAA2020032508933Stiffener · crackedCRACKED VERTICAL STIFFENER AT B.S.663 LOWER COMPOSITE BULKHEAD; ON AFT SIDE; L.B.L 25; W.L. 150. / REMOVED & REPLACED VERTICAL STIFFNER AT BS663 LBL-25 IAW SRM 51-40-02 & DWGS 111A1000 REV.-; 149A7210 REV.B. 59191U;17MAR2020.SDR SWAA2020040936735Structure · dentedFLIGHT DECK FLOOR IS DENTED AT B.S. 255; L.B.L. 3 - L.B.L. 12; W.L. 207.54. / REPAIRED FLIGHT DECK FLOOR BS 255 LBL 3-LBL12 WL 207.54 PER ATS ER #20-02160 REV IR AND EA 1-753-36792 REV IR.SDR SWAA2020012240674Connector · faultyDECLARED EMERGENCY, UPON INITIAL FLAP EXTENSION ONLY 1/2 DEGREES OF FLAPS CAME OUT. ALSO THERE WAS AN ASYMMETRY CONDITION. LEADING EDGE. DEVICES DID NOT EXTEND. FOLLOWED QRH PROCEDURES FOR TRACKING EDGE FLAP / ASYMMETRY LEADING US TO TRACKING EDGE FLAPS UP SDR SWAA2020012040557Slide · out of limitsR2 DOOR SLIDE WAS BELOW SERVICEABLE LIMIT. R&R SLIDE IAW MT.SDR SWAA2019123140035Screw · missingOVER WING EMERGENCY EXIT DOOR ON CAPTAINS SIDE LOWER HANDLE AND COVER ASSEMBLY BROKEN. / INSTALLED MISSING HARDWARE IAW SIP.SDR SWAA2019121839782Outflow Valve · faultyDECLARED EMERGENCY--------------------------------------------------WHILE DESCENDING THROUGH 30,000 / FT. CABIN RATE INCREASED AT 4000 FPM OR GREATER. CABIN CLIMBED THROUGH 10,000 FT. PERFORMED A RAPID DEPRESSURIZATION DESCENT AND ACCOMPLISHED THE QRC "CABINSDR SWAA2019120939436Cover · detachedL/H EMERGENCY LIGHT COVER FELL OFF AT ROW 14. / SECURED COVER PER SIP.SDR SWAA2019120339273Light · inoperativeR1 DOOR EXIT LOCATOR SIGN INOP. / R&R LIGHT ASSEMBLY PER AMM.SDR SWAA2019120339272Wire · disconnectedL/H WING OVER EMERGENCY EXIT LOCATOR SIGN INOP. / CONNECTED WIRE PER WDM AND AMM..SDR SWAA2022032403139Retainer · crackedL/W AFT TIP OF THE #1 PYLON BULB SEAL RETAINER IS CRACK. / REMOVED ADN REPLACED L/W AFT #1 PYLON CURVED BULB SEAL RETAINER IAW SRM 51-40-02-0G-0. 57055U 24NOV19SDR SWAA2019112639136Power Supply · malfunctionedFORWARD CABIN, EMERGENCY EXIT LIGHTS COMMON TO M1675 WERE NOT OPERATING CORRECTLY. / R&R POWER SUPPLY IAW AMM.SDR SWAA2019112639118Battery Pack · malfunctionedFORWARD CABIN, EMERGENCY EXIT LIGHTS COMMON TO M1675 WERE NOT OPERATING CORRECTLY. / R&R BATTERY PACK IAW AMM.SDR SWAA2019112539106Channel · corrodedR2 DOOR MOPSILL CORRODED BETWEEN BS. 947 TO BS. 992, STR. 17R. / R&R MOPSILL IAW SRM & DWG.SDR SWAA2022032303119Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 241AAF DELAMINATING / DUE TO EXTENT OF FIBER DAMAGE; FABRICATED A REPLACEMENT PANEL FOR 241AAF USING BMS 4-17 TY 6 LOT #1409148-1 & BMS 5107 LOT# AK9FP3008K IAW SRM 53-00-50-2R-0 & DWG 147A5810-8 7062U 11-18-19SDR SWAA2022032303113Panel · delaminatedL/W L/E PANEL 521SB DELAMINATED ON CORNER (MARKED) / REPAIRED DELAMINATED (MARKED) L/W L/E ON PANEL 521SB IAW SRM 57-41-01-2R-6 & 51-70-05-2R-6 7063U 11-22-19SDR SWAA2019112639103Rib · crackedR/H HORIZONTAL STABILIZER LEADING EDGE HAD CRACKED RIB AT LEADING EDGE STA. 114.55. / R&R RIB IAW SRM & DWG.SDR SWAA2019112539105Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 241ADF DELAMINATED, BETWEEN BS. 887 TO BS. 1016. / REPAIRED FLOOR PANEL 241ADF IAW SRM.SDR SWAA2019112539104Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 242VF DELAMINATED BETWEEN BS. 887 TO BS. 1016. / REPAIRED FLOOR PANEL 242VF IAW SRM.SDR SWAA2019112539070Rib · crackedR/H HORIZONTAL STABILIZER LEADING EDGE HAD CRACKED RIB AT LEADING EDGE STA. 105.26. / R&R RIB IAW SRM & DWG.SDR SWAA2019112539069Rib · crackedR/H HORIZONTAL STABILIZER LEADING EDGE HAD CRACKED RIB AT LEADING EDGE STA. 86.6. / R&R RIB IAW SRM & DWG.SDR SWAA2019111838894Anti-Skid Valve · faultyDECLARED EMERGENCY-------------------------------------------------------ANTI-SKID INOP LIGHT CAME ON DURING THE DESCENT INTO KSAN AND REMAINED ON THROUGH LANDING INTO KSAN. / R&R #3 ANTI SKID VALVE IAW AMM.SDR SWAA2022040666455Intercostal · corrodedCUSTOMER REQUEST: (F.B.) AFT CARGO COMPARTMENT INTERCOSTAL BS 787-807 AT S-27R IS CORRODED. WL 156 / INTERCOSTAL WAS FOUND TO HAVE 100% MATERIAL LOSS. REMOVED AND REPLACED NTERCOSTAL AT STA 787-807 STR 27R IAW BOEING DWG #146A8130 REV: B AND SRM 51-40-02-0G-0.SDR SWAA2022033166456Stiffener · crackedLH VAPOR BARRIER HORIZNAL STIFFNER AT LBL 6-30 AND AT STA.663 CRACKED / REMOVED HORIZ STIFFENER AT BS 663; LBL 6 TO 3D IAW SRM 51-40-02-0G-0. FABRICATAED NEW STIFFENER IAW EA 190941 REV. IR AND SWA EA 1-757-16681 REV. IR. INSTALLED NEW STIFFENER IAW SRM 51-40-SDR SWAA2019111438828Angle · crackedUPPER VAPOR BARRIER FORWARD SUPPORT ANGLE, CENTER FUEL TANK CRACKED AT BS. 663, LBL 7. / REPAIRED ANGLE IAW SRM.SDR SWAA2022040566445Panel · crackedRW PANEL 651 GB HAS A CRACK ON FWD O/B SIDE OF BRACKET MARKED IN RED. / DAMAGED BRACKET TO RW PANEL 651GB REMOVED AND REPLACED NEW IAW B-737 SRM 51-40-02-0G-0. NEW PART FASTENER LOCATIONS LOCATED AND DRILLED IAW B-737 SRM 51-40-05-0G-0; SRM 51-40-06-0G-0; & 51SDR SWAA2019111338812Crease Beam · corrodedL/H CREASE BEAM AT FORWARD ENTRY, CORRODED FROM LOWER FORWARD CUTOUT TO AFT LOWER CUTOUT. / R&R L-1 CREASE BEAM CHORD IAW SRM & DWG.SDR SWAA2022040566440Floor Panel · corrodedAFT CARGO FLOOR PANEL 140DF HAS CORROSION FWD LOWER EDGE / FABRICATECD NEW FLOOR PANEL 140DF IAW IPC 25-52-10-02 AND BOEING DWG 453A2610 REV: B. EA 190924 REV. P1 CANCELLEDSDR SWAA2022030166435Balance Weight · corrodedRUDDER BALANCE WEIGHT HAS HEAVY CORROSION ON FWD SIDE._RUDDER STATION 151.17; 17.05 INCHES FWD OF HINGE C/L / REMOVED & REPLACED RUDDER BALANCE WEIGHT IAW CMM 55-40-09 DISASSEMBLY & ASSEMBLY P/N 173A5103-1SDR SWAA2022040566430Bracket · crackedAFT ENTRY DOOR PANEL 834DZ AFT BRACKET CRACKED / REMOVED & REPLACED BROKEN L2 DOOR PANEL 834DZ AFT BRACKET W NEW PN 411A2129-548 IAW AIPC 52-13-21-10 & SRM 51-40-02-0G & ATAG # A60238SDR SWAA2022040566429Bracket · crackedAFT GALLEY DOOR PANEL 844DZ AFT BRACKET CRACKED / REMOVED & REPLACED BROKEN R2 DOOR PANEL 844DZ W/ NEW BRACKET PN 411A2129-547 IAW AIPC 52-41-31-10 SRM 51-40-02-0G-0 SRM 51-40-05-0G-0 ATAG# A60235SDR SWAA2022040566427Panel · delaminatedRT WING; LWR L/E PANEL 621DB HAS THREE CORNERS DELAMINATED. / VERIFIED NEW PART #116A9110Y30 FOR RIGHT WING; LOWER L/E PANEL 621DB; ATAG# FT2584. LOCATED; DRILLED; COUNTERSUNK NEW FASTENER LOCATIONS IN BLANK PANEL IAW SRM 51-40-05-0G-0 AND SRM 51-40-08-0G-0
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