N8669B
Service difficulty reports · 65
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 = 'N8669B' 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 = 'N8669B' 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 SWAA2026051903519Bulb · burned outAFT RIGHT UPPER INTERIOR SERVICE DOOR EMERGENCY EXIT LIGHT 1 BULB OUT. RELAMPED AND PERFORMED GOOD OPS CHECK IAW AMM 33-51-01-960-801.SDR SWAA2026033184153Megaphone · inoperativeFWD GALLEY MEGAPHONE INOP. REMOVED AND REPLACED FWD GALLEY MEGAPHONE IAW AMM 25-64-00. OPS CHECK GOODSDR SWAA2026021267550Lamp · inoperativeR2 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IN THE EMERGENCY LIGHT AND OPS CHECKED GOOD IAW AMM 33-54-01.SDR SWAA2025061379494Egt Indication · illuminatedAFTER ROTATION THE NUMBER 2 ENGINE EXCEEDED THE EGT LIMITATION. THE EGT WAS SOLID RED AND WE SAW 906 COMPLETED QRH ENGINE CONSISTENTLY RAN 50-60 HIGHER THAN NUMBER 1 ENGINE BUT WITHIN NORMAL PARAMETER<[01] C/W EA 25-171-01518;[02] ENTERING CORRECT SELECT REFERSDR SWAA2024112161105Light · looseMID CABIN CEILING EMERGENCY EXIT SIGN IS LOOSE<[01] RE ADJUST EXIT LIGHT ASSEMBLY PER AMM 33-51-01.SDR SWAA2024071613054Flap System · malfunctionedFLAPS DID NOT EXTEND BEYOND FLAPS 5 WHILE ON APPROACH ; FLAP HANDLE IN THE FLAPS 30 POSITION<[01] REF LOG 2595068 FLAP OVER SPEED - PERFORMED FSEU BITE PER FIM 27-51 TASK 801; NO EXISTING FAULTS FOUND; NO LAST LEG FAULT HISTORY. PERFORMED FLAP TRANSMISSION TORSDR SWAA2024071611221Battery Pack · inoperativeEMERGENCY LIGHT BATTERY AT M01673 WILL NOT CHARGE<[01] REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-06-960-805 OPS CHECK GOOD;[02] VERIFIED ITEM 1<BR><BR>AUDIT C/WSDR SWAA2024071511218Battery Pack · inoperativeEMERGENCY LIGHT BATTERY AT M01695 WILL NOT CHARGE<[01] REMOVED AND REPLACED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)];[02] REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-06-960-805 OPS CHECK GOOD;[03] VERIFIED STEPS 1SDR SWAA2024071511220Battery Pack · inoperativeEMERGENCY LIGHT BATTERY AT M01672 WILL NOT CHARGE<[01] REMOVED AND REPLACED IAW [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)];[02] REMOVED AND REPLACED IAW AMM 33-51-06-960-805-NG CHECK OPS GOOD;[03] REMOVED AND REPLACED BATTESDR SWAA2024071511222Battery Pack · inoperativeEMERGENCY LIGHT BATTERY AT M01675 WILL NOT CHARGE<[01] REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-06-960-805. OPS CHECK GOOD.;[02] VERIFIED ITEM 1<BR><BR>AUDIT C/WSDR SWAA2024071511219Battery Pack · inoperativeEMERGENCY LIGHT BATTERY AT M02816 WILL NOT CHARGE<[01] REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-06-960-805. OPS CHECK GOOD.;[02] VERIFIED ITEM 1<BR><BR>AUDIT C/WSDR SWAA2024071511109Lens · wornEMERGENCY EXIT LIGHT ON G1 GALLEY IS WORN<[01] REMOVED AND REPLACED G1 GALLEY EMERGENCY EXIT LIGHT LENS IAW AMM 33-51-01-960-802-NG STEPS 3E(1(A2)) AND 3E(2(G2)) OP CHECK GOOD<BR>A-TAG; WN31349;[02] VERIFIED ITEM 1<BR><BR>AUDIT C/WSDR SWAA2024071110063Erosion Shield · delaminated(A150-001) CORNER DELAMINATED ON LEFT WING L/E PANEL 521TB.<[01] BONDED LOOSE EROSION STRIP IAW SRM 57-41-01-2R-6;[02] AUDITSDR SWAA2024071505882Plate · failed(A-221 DOT 38); FWD WET AREA L1 DOOR IS SAGGING/ FAILED GAP CHECK BETWEEN DOOR AND DOOR SKIN CUTOUT<[01] REMOVED AND REPLACED UPPER AND LOWER SERRATED PLATE ASSEMBLIES; AND GUIDE ARM IAW SRM 51-40-02-0G-0 AND TASK CARD 752-RCB-01-01 FAULT TTG8R007P3ND. L1 DOORSDR SWAA2023080986918Slide · out of adjustAFT LEFT SERVICE DOOR SLIDE HAS A BLACK ELECTRICAL CORD HANGING OUT<[01] UPON INSPECTION FOUND TO BE SLIDE TEST CONNECTOR; SECURED CONNECTOR BACK INTO SLIDE SLEEVE AS REQUIRED REF S.I.P AND AMM 25-66-01SDR SWAA2023061956956Slat · cracked#4 SLAT MID FLEX SKIN CRACKED<[01] REMOVED AND REPLACED FLEX SEAL (SKIN) IAW SRM 51-40-02SDR SWAA2023061956953Battery Pack · inoperativeSEVERAL CABIN EMERGENCY LIGHTS INOP. BOTH SIDES BULL NOSE LIGHTS<[01] REMOVED AND REPLACED 5 EACH BATTERY PACKS IN CABIN FOR BULL NOSE EMERGENCY LIGHTS PER MM 33-51-06; OPS CHECKS GOOD PER MM 33-51-00;[02] REMOVED AND REPLACED 5 EACH BATTERY PACKS IN CABIN FORSDR SWAA2023061952600Angle · crackedAFT CARGO FLOOR STRUCTURE: LEFT SIDE PLATE (TRANSITION ANGLE) IS CRACKED AT STA 727J +9. MARKED.<[01] AFT CARGO L/H TRANSITION ANGLE AT STA 727J +9 TO BE REPLACED ON FAULT TTG8Q00L9SR4.;[02] VERIFIED.SDR SWAA2023061952611Angle · corrodedAFT CARGO FLOOR STRUCTURE: LEFT SIDE PLATE (TRANSITION ANGLE) HAS CORROSION AROUND THE FASTENER HOLES. LOCATED AT STA 727J +2; +6; +13 AND +14. MARKED. AFT CARGO FLOOR STRUCTURE: LEFT SIDE PLATE (TRANSITION ANGLE) HAS CORROSION AROUND THE FASTENER HOLES. LOCATSDR SWAA2023061952595Splice · corrodedAFT CARGO FLOOR STRUCTURE: CORROSION ON THE UPPER SURFACE OF FLOOR SUPPORT BEAM. LOCATED AT STA 787 RBL 15 ABOVE STR 26R. MARKED. SEE ATTACHED IMAGES.<[01] COMPLIED WITH TOOL REQUIREMENT.;[02] COMPLIED WITH MEASUREMENTS.;[03] REMOVED CORROSION FROM AREA PER SRSDR SWAA2023061952609Web · corrodedAFT CARGO FLOOR STRUCTURE: CARGO DOOR THRESHOLD SUPPORT WEB HAS CORROSION ON THE UPPER SURFACE AROUND FASTENERS HOLES STARTING AT STA 787 THROUGH STA 847 RBL 22 TO RBL 26. MARKED (SEE ATTACHED IMAGE.)<[01] DAMAGE OUT OF LIMITS PER SRM 53-60-15-1A-1;[02] CONFIRSDR SWAA2023061952589Floorbeam · corrodedAFT GALLEY STA. 947.5 LBL 24.75 CORROSION AROUND TIE-DOWN FITTING.<[01] CORROSION DAMAGE OUT OF LIMITS PER SRM 53-70-51-1A-1;[02] VERIFIED CORRECTIVE ACTION STEP #1;[03] CUTOUT DAMAGED UPPER CHORD OF FLOOR BEAM AT STA 947.5 FROM LBL 9 TO LBL 42 PER SRM 53-70-5SDR SWAA2023061952592Intercostal · corrodedFWD LAV; AFT IB MOUNT AT STA 303.9 LBL 13 HAS CORROSION UNDER NUTPLATE.<[01] REMOVED FWD LAV. AFT I/B MOUNT FITTING AND NUT PLATE PER SRM 51-40-02.<BR>BLENDED OUT CORROSION AT LAV ATTACH FASTENER HOLE PER SRM 51-10-02. FOUND PITTING AND CRACK WITHIN FASTENER HSDR SWAA2023061952583Floorbeam · corrodedAFT GALLEY STA. 987 FLOORBEAM RBL 43 HAS CORROSION AROUND NUT-PLATE HOLE.<[01] CORROSION DAMAGE OUT OF LIMITS PER SRM 53-70-51-1A-1;[02] VERIFIED CORRECTIVE ACTION STEP #1;[03] CUT OUT DAMAGE AREA PER SRM 53-70-51-2R-6 REPAIR ALTERNATIVE 4.;[04] PERFORMED HIGHSDR SWAA2023061952037Flap · delaminatedRIGHT HAND WING OUTBOARD AFT FLAP IS DELAMINATED ON THE INBOARD END.<[01] REMOVED R/H WING 'O/B AFT FLAP' IAW AMM 27-51-22.;[02] INSTALLED SERVICEABLE R/H O/B AFT FLAP REF AMM 27-51-22;[03] RII: INSPECTED WORK ACCOMPLISHED IN C/A# 2. THOMAS TESTEMENT (TECHNICISDR SWAA2023061952038Flap · delaminatedLEFT HAND WING OUTBOARD AFT FLAP IS DELAMINATED ON THE INBOARD END.<[01] REMOVED L/H WING; ' O/B AFT FLAP '; IAW AMM 27-51-22.;[02] ACCOMPLISHED INSTALLATION OF L/H WING; ' O/B AFT FLAP ' IAW AMM 27-51-22-400-801 UP TO AND INCLUDING STEPS 3. A;B;C;D;E; AND F. SDR SWAA2023061952046Flap · delaminatedRIGHT HAND INBOARD MAIN FLAP TRAILING EDGE WEDGE HAS LARGE AREA OF DELAMINATING (MKD)<[01] REMOVED DELAMINATED R/H I/B MAIN FLAP T/E WEDGE PER SRM 51-40-02.;[02] REMOVED PART FROM INVENTORY;[03] OKAY TO CLOSE RIGHT HAND INBOARD MAIN FLAP TRAILING EDGE WEDGE;[0SDR SWAA2023061950703Lens · damagedPASSENGER COMPARTMENT EMERGENCY EGRESS LIGHT FIXTURE AT SEAT ROW 21DEF HAS DAMAGE.<[01] R&R'D EMERGENCY EGRESS LIGHT LENS PER AMM 33-51-03;[02] C/W.SDR SWAA2023020900579Lens · looseEMERGENCY EXIT LENS CAME OFF<[01] SECURED LENS I/A/W S.I.P.SDR SWAA2023010386686Battery Pack · inoperativeL/H OVERWING EXIT EMERGENCY LIGHTS INOP.<[01] R/R EMERGENCY LIGHT BATTERY PACK REF AMM 33-51-06; OPS CHK GOOD.SDR SWAA2022112374765Seal · crackedR/H HORIZONTAL STAB UPPER FWD SLIDER SEAL IS CRACKED. REMOVED AND REPLACED R/H HORIZONTAL STABILIZER UPPER FWD SLIDER SEAL PER AMM 53-31-31.SDR SWAA2022112374766Seal · crackedL/H HORIZONTAL STAB UPPER FWD SLIDER SEAL IS CRACKED. REMOVED AND REPLACED L/H HORIZONTAL STAB UPPER FWD SLIDER SEAL PER AMM 53-31-31.SDR SWAA2022111772470Battery Pack · inoperativeONE INTERIOR EMERGENCY LIGHT INOP AT AFT LT OVHD BIN. EMERGENCY BATTERY PACK M1673 REPLACED. OPS CHECKED NORMAL IAW AMM 33-51-06-960-805.SDR SWAA2022111772469Battery Pack · inoperativeINTERIOR EMERGENCY LIGHTS INOP AT L2 DOOR. EMERGENCY BATTERY PACK POS. M1673 WAS REPLACED. PERFORMED OPS CHECK OF THE INTERIOR EMERGENCY LIGHTS AT L2 DOOR AND FOUND NORMAL IAW AMM 33-51-06-960-805.SDR SWAA2022111772468Battery · inoperativeEXTERIOR EMERGENCY LIGHTS INOP AT R2 DOOR. EMERGENCY BATTERY PACK POS. M1673 WAS REPLACED. PERFORMED OPS CHECK OF THE EXTERIOR EMERGENCY LIGHTS AT R2 DOOR AND FOUND NORMALSDR SWAA2022111772467Battery · inoperativeEXTERIOR EMERGENCY LIGHTS INOP AT L2 DOOR. REMOVED AND REPLACED EMERGENCY BATTERY PACK POS M1673. PERFORMED OPS CHECK FOUND NORMAL. REMOVED AND REPLACED EMERGENCY BATTERY PACK POS M1673 PER REF AMM 33-51-06-960-805. PERFORMED OPS CHECK FOUND NORMAL.SDR SWAA2022053112522Pump · faultyON TAKEOFF WITH TOGA SEL #1 ENG WENT TO 93.5 % N1; #2 ENGINE WENT TO 87.4% N1. ADVANCING (MANUALLY) THE #2 THRUST LEVER DID NOT ADVANCE N1 ABOVE 87.4%. / [01] AFTER INSTALLATION OF FUEL PUMP PACKAGE; #2 ENGINE TAKEOFF POWER IS SATISFACTORY; IAW B737 AMM 71-00-SDR SWAA2021122154220Seal · out of positionRT HORIZONTAL STABILIZER AFT UPPER SLIDING SEAL OUT OF CHANNEL ; / [01] RE-POSITIONED SEAL PER AMM 27-41-11 STEP G 15SDR SWAA2021110941494Battery Pack · inoperativeELECTRICAL FUMES SMELL AROUND ROW 4; NO ABNORMAL ENG INDICATIONS ; / [01] ACCOMPLISHED CONDITIONAL INSP PER AMM 05-51-56 AND FIM 21-00 TASK 806 PARA. C;G;H;I; AND J. NO FAULTS FOUND. COULD NOT DUPLICATE CONDITION. INSPECTED PSUS AND OVERHEAD BINS IN SUSPECT ROSDR SWAA2021110941350Power Supply · inoperativeELECTRICAL FUMES SMELL AROUND ROW 4; NO ABNORMAL ENG INDICATIONS ; / [01] ACCOMPLISHED CONDITIONAL INSP PER AMM 05-51-56 AND FIM 21-00 TASK 806 PARA. C;G;H;I; AND J. NO FAULTS FOUND. COULD NOT DUPLICATE CONDITION. INSPECTED PSUS AND OVERHEAD BINS IN SUSPECT ROSDR SWAA2021110137756None · looseEXIT SIGN COVER AFT OF EMERGENCY EXIT DOOR ROW 15 BC IS LOOSE / SECURED EXIT SIGN COVER PER SIPSDR SWAA2021070688442Battery Pack · inoperativeFWD GALLEY L/H EMERGENCY LIGHT INOP / R&R FWD GALLEY L/H EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-06POS 1: P/N OFF/ON: D717-01-100S/N OFF: 403902 S/N ON: 403902SDR SWAA2021070687237Skin · crackedR/H I/B FLAP I/B END ELEPHANT EAR WORN AND CRACKED LOWER SIDE (MARKED) / REMOVED AND REPLACED THE ELEPHANT EAR ON THE R/H I/B FLAP; I/B END IAW AMM 27-51-11SDR SWAA2021070685445Battery Pack · inoperativeAFT SERVICE DOOR EMERGENCY EXIT LIGHT ON HEADER PANEL AND R/H OF G-4 GALLEY DOES NOT ILLUMINATE DURING OPERATIONAL TEST / REMOVED AND REPLACED AFT SERVICE DOOR EMERGENCY EXIT LIGHT BATTERY PACK IAW AMM 33-51-06. OPS CK GOOD.INSP D54SDR SWAA2021070682757Attach Angle · corrodedATTACH ANGLE LOCATED UNDER TRANSITION ANGLE (SHIELD) FROM STA 767 TO 787 AND RBL 21 HAS CORROSION AROUND AND UNDER NUTPLATES. / REMOVED AND REPLACED ATTACH ANGLE UNDER TRANSITION ANGLE (SHIELD) P/N # 146A8127412 ATSMROPER SRM. 51-40-02 (SA-M 326 ATTACHED: A130SDR SWAA2021070680860Intercostal · crackedL/H WING; INTERCOASTAL CRACKED INBD OF DEFLECTION / REMOVED & REPLACED DAMAGED INTERCOASTAL PER SRM 51-40-02.(SA-M 326 A1303118)SDR SWAA2021070680910Control Panel · faultyFUEL PANEL OPENING 532DB EDGES ARE NOTCHED FROM PANEL BOLTS / ACCOMPLISHED REPAIR TO FUEL PANEL OPENING 532DB IAW SRM 57-50-01-1A-1 AND SRM 57-20-01-2R-1 REPAIR 1.REFERENCE AP37.8.0615 SRM SUPPLEMENT AVIATION PARTNERS BOEING 57-20-01 REPAIR 1.SDR SWAA2021070680911Control Panel · faultedFUEL PANEL OPENING 532PB EDGES ARE NOTCHED FROM PANEL BOLTS / ACCOMPLISHED REPAIR TO FUEL PANEL OPENING 532PB IAW SRM 57-20-01-1A-1 AND SRM 57-20-81-27-1 REPAIR 1.REFERENCE AP37.8.0615 SRM SUPPLEMENT AVIATION PARTNERS BOEING 57-20-01 REPAIR 1.SDR SWAA2021070679831Angle · corrodedFWD CARGO LEFT T- ANGLE HAS CORROSION ON SURFACE @ STA 500+15 LBL 24 / REMOVED AND REPLACED LEFT TRANSITION ANGLE FROM STA 480 + 9 TO 500 I PER SRM 53-00-53-2R5 AND EA #21-153-01621 REF SRM ID 53-30-53-0I-2 FIG 2 TABLE 2 INTEM 6 143A7501 CHANNEL # BAC1496-444SSDR SWAA2021070679828Angle · corrodedFWD CARGO RIGHT TRANSITION ANGLE HAS SURFACE CORROSION FROM STA 500 TO STA 500A RBL 35 . / REMOVED AND REPLACED FWD CARGO RIGHT TRANSITION ANGLE FROM STA. 500 TO STA. 500A AT RBL 25' PER SRM 51-40-02.(SA-M 326 ATTACHED: A1303121)
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