N165AW, cancelled May 20, 2002
Service difficulty reports · 75
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 = 'N165AW' AND deregistration_id = 'N165AW-2002-05-20' 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 = 'N165AW' AND deregistration_id = 'N165AW-2002-05-20' 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 M522001F00000Pressure Panel · crackedLEFT HAND W/W FUS STATION 664.0 PRESSURE WEB CRACKED IN 1 LOCATIONS LBL 34.SDR AWXA0002004Indicator · failedPHX -AIR TURNBACK- FLT 173- AFTER TAKEOFF FROM PHX THE NR 1 ENGINE EGT INDICATOR WENT TO ZERO AND THE AIRCRAFT RETURNED TO PHX. THE AIRCRAFT LANDED OVERWEIGHT AT 124.3 THOUSAND LBS AND 200 FPM SINK RATE. AN OVERWEIGHT LANDING INSPECTION WAS PERFORMED WITH NOSDR AWXA0001887Nut · looseIAH-AIR TURNBACK- INFLIGHT SHUTDOWN - FLT 831- DURING CLIMB THE NR 1 ENGINE EGT INDICATOR RED LIGHT ILLUMINATED. THE DIGITAL AND ANALOG EGT INDICATIONS SHOWED EXCESSIVE EGT. THE INDICATIONS WERE ERRATIC AND VARIED BETWEEN 700 AND OFF SCALE, OVER 1000. THE ESDR AWXA0001483Fire Loop · out of positionPHX - AIR TURNBACK - 3/5/01 - ON CLIMBOUT AT FL270 W/ FULL POWER, THE RT WING BODY OVERHEAT LIGHT ILLUMINATED; W/ THE ISOLATION VALVE CLOSED AND RIGHT BLEED OFF THE LIGHT EXTINGUISHED. MAINTENANCE TROUBLESHOT AND FOUND FIRE LOOP IN NR 2 PYLON TO CLOSE TO THE SDR AWXA0001149Skin · crackedLIGHT AFT OF RT AFT WING-BODY FAIRING HAS TEMP REPAIR DOUBLER BS 727D STR 23R. REMOVED TEMP DOUBLER, FABED REPAIR PARTS AND INSTALLED IAW ER 03-5361-00347-001 AND SRM 53-00-01SDR AWXA0001148Bracket · brokenRT A/C EXHAUST LOUVER MOUNT BRACKETS BROKEN. REMOVED, FABED REPLACEMENT BRACKET, INSTALLED IAW SRM 51-40-02 AND SRM 51-30-01SDR AWXA0001147Floorbeam · corrodedFS 312 RBL 6 - RBL 12 FLOOR BEAM UPPER CHORD CORRODED OUT OF LIMITS. CUT OUT DAMAGED CHORD LBL 6 - RBL 26 AND REPAIRED IAW SRM 53-10-51 FIG 205SDR AWXA0001146Bracket · brokenLT A/C EXHAUST LOWER MOUNT BRACKETS BROKEN. REMOVED, FABED REPLACEMENT BRACKET, INSTALLED IAW SRM 51-40-02 AND SRM 51-30-01SDR AWXA0001145Skin · crackedLT PYLON SKIN CRACKED AT ACCESS PANEL 5727L. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW SRM 54-50-01, S/B 737-54-1035SDR AWXA0001144Skin · corrodedLIGHT SURFACE CORROSION ON LT WING LOWER SKIN AT ACCESS PANEL 7212 FLANGE. REMOVED CORROSION W/I LIMITS IAW SRM 57-20-01 FIG 205; SHOT PEENED IAW 51-20-06 FIG 1; TREATED AND PRIMED IAW 51-20-01SDR AWXA0001143Skin · crackedLT O/B WING AFT FLAP L/E DEEP CHAFE WITH CRACK AT O/B ROLLERS. REMOVED DAMAGE, FABED AND INSTALLED REPAIR PARTS SKIN & SPLICE IAW SRM 57-53-01 FIG 204.SDR AWXA0001135Stiffener · crackedNR 6 FLAP TRACK FAIRING STIFFENER AND DOUBLER CRACKED. REMOVED RT. WING I/B FLAP ASSY BOTTOM I/B STIFFENER AND DOUBLER IAW SRM 51-40-02; INSTALLED NEW STIFFENER AND DOUBLER IAW 51-40-02SDR AWXA0001134Skin · crackedLEFT I/B AFT FLAP LEADING EDGE CRACKED AT 3RD HINGE OBD. REMOVED LEADING EDGE IAW SRM 51-40-02; CUTOUT DAMAGED PORTION IAW 57-53-01; FABED SKIN REPAIR AND SPLICE PLATE IAW 57-53-01; TREATED AND PRIMED REPAIR PARTS IAW 51-20-01; INSTALLED PARTS AND SEALED IAW 5SDR AWXA0001133Skin · brokenFLANGE ON A/C GROUND CONNECT BROKEN (INNER FLANGE INNER DOUBLER) ON FUSELAGE SKIN AT DOOR LANDING RING. CUT OUT DAMAGED FLANGE; HFEC SHOWS NO CRACKS; FABED REPAIR PLATE; PRIMED AND TREATED ALL FAY SURFACES; INSTALLED REPAIR PLATE AND CONICAL WASHERS IAW SRM 53SDR AWXA0001132Skin · corrodedLIGHT SURFACE CORROSION ON LT WING LOWER SKIN AT ACCESS PANEL 7211 FLANGE. REMOVED CORROSION W/I LIMITS IAW SRM 57-20-01 FIG 205; SHOT PEENED IAW 51-20-06 FIG 1; TREATED AND PRIMED IAW 51-20-01 AS REQUIRED.SDR AWXA0001131Bulkhead · crackedULTRASONIC INSP. DETECTED CRACK APPROX. 4.0 INCHES LONG AT FWD PRESSURE BULKHEAD AT STA 178 WL 213 BETWEEN LBL 5 & LBL 17 ON WEB BEHIND HORIZ ANGLE STIFFENER. REMOVED ANGLE, STOP DRILLED CRACK IAW SRM 53-10-08; CRACK TERMINATED; FABED DOUBLER AND SHIMS IAW 53-SDR AWXA0001130Frame · crackedCABIN RT I/B FWD OVERWING EXIT FRAME SUPPORT CRACKED AT BOTTOM FASTENER HOLE AREA BS 616 BELOW CABIN FLOOR PANEL STR 17R. REMOVED FASTENERS AND COLLARS IAW ER 03-5310-00339-JS1; CUT OUT DAMAGED AREA FROM FRAME IAW ER 03-5310-00339-JS1; NDT INSPECTED CUT OUT HFSDR AWXA0001129Strap · crackedFS 178 WL 187 BL 0 STRAP CRACKED. REMOVED STRAP; FABED REPAIR STRAP AND DOUBLER IAW SRM 51-70-13 FIG 1SDR AWXA0001128Seat Track · corrodedCABIN SEAT TRACK RBL 24 I/B FLANGE HAS BARE METAL ON UNDERSIDE AT EACH FLOOR BOARD FASTENER HOLE - SOME WITH LIGHT SURFACE CORROSION - FROM BS 540 - 727. REMOVED LIGHT SURFACE CORROSION - .070 MATERIAL LOSS .001-.002 FOUND WITH IN LIMITED MECHANICAL MEASUREMENSDR AWXA0001127Channel · corrodedCORROSION ON RT AFT LAV WALL LOWER SUPPORT CHANNEL STA 993 FROM RBL 23 - RBL 44 WAS FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED HAT SECTION IAW SRM 51-40-02; FABED HAT SECTION IAW DWG 65C19883 AND SRM 51-30-01; ALODINED AND PRIMED IAW 51-20-01; INSTALLED HAT SESDR AWXA0001126Web · crackedFLOOR WEB CRACKED FS 180 WL 207 LBL 26 (1.0L). REMOVED DAMAGED WEB; FABED NEW WEB; INSTALLED WEB IAW SRM 51-40-02 DWG 65-45833SDR AWXA0001124Skin · crackedNR 1 SLAT HAS CRACKS IN AFT ROW OF RIVETS LWR SURFACE, INBD OF ACTUATOR. REMOVED DAMAGED AREA; FABED AND INSTALLED REPAIR PARTS, FILLER AND SPLICE PLATE IAW SRM 57-43-01 FIG 206SDR AWXA0001123Skin · scratchedFUSE SKIN FROM STA 1060-1070 L14L HAS DEEP SCRATCH UNDER W OF TAIL NUMBER; FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SKIN; NDT NO CRACKS NOTED; FABED REPAIR PLATE; INSTALLED PLATE; INSTALLED CONICAL WASHERS IAW SRM 53-00-01, 51-40-02.SDR AWXA0001122Web · crackedFLOOR WEB CRACKED FS 180 WL 207 RBL 26 (1.0L). REMOVED DMGD WEB IAW SRM 51-40-02; FABED REPLACEMENT WEB IAW DWG 65-45833; INSTALLED IAW 51-40-02SDR AWXA0001121Frame · crackedSIDE CHORD CRACKED FS 178 WL 207 LBL 26 (1.6L) AND WL 195 LBL 24 (1.3L). CUTOUT CRACKED SECTION OF CHORD WL 212-175 IAW ER 03-5310-00339-JS3; NDT NO CRACKS NOTED IAW 51-00-00 FIG 23; FABED AND INSTALLED REPAIR PARTS IAW ER 03-5310-0039-JS3SDR AWXA0001120Web · crackedCENTER WEB CRACKED FS 178 WL 187 LBL 0.7 AND RBL 0.7. REMOVED DAMAGED AREA; FABED AND INSTALLED REPAIR PARTS IAW SRM 53-10-08 FIG 203SDR AWXA0001119Web · crackedCENTER WEB CRACKED FS 178 RBL 5.0 WL 198 (1.3L) AND WL 202 (0.9L). REMOVED DAMAGE; FABED AND INSTALLED REPAIR PARTS IAW SRM 53-10-08 FIG 209SDR AWXA0001115Frame · gougedRT MLG WHEEL WELL, AFT CUTOUT VERTICAL ANGLE BRACKET GOUGED (LOCATED ADJACENT TO GROUNDING STUD). REMOVED RT HYD PANEL COVER MAIN LANDING GEAR RIGHT SIDE IAW SRM 51-40-02; REMOVED RT OUTBOARD AFT MAIN LANDING GEAR PANEL IAW 51-40-02; REMOVED AND REPLACED DAMAGSDR AWXA0001114Stiffener · crackedLT WING LWBL 184 TE AT NR 3 FLAP TRACK FAIRING INBOARD FORMER/STIFFENER CRACKED. REMOVED AND REPLACED STIFFENER IAW SRM 51-40-02SDR AWXA0001113Bulkhead · crackedCENTER WEB CRACKED FS 178 LBL 5.0 WL 198 & 202. REMOVED DAMAGE, FABED AND INSTALLED REPAIR PARTS IAW SRM 53-10-18 FIG 209SDR AWXA0001112Intercostal · crackedINTERCOSTAL CRACKED THRU FS 178 WL 195 RBL 24. REMOVED INTERCOSTAL IAW SRM 51-40-02; CUTOUT DAMAGE IAW 53-10-08 FIG 202; HFEC INSPEC IAW B737 NTM PT.6 51-00-00 FIG 23 NO CRACKS NOTED; REPAIRED INTERCOSTAL WITH FILLER, ANGLE, AND RADIUS BLOCK; INSTALLED IAW SRMSDR AWXA0001111Intercostal · crackedINTERCOSTAL CRACKED THRU FS 178 WL 195 LBL 24. REMOVED INTERCOSTAL IAW SRM 51-40-02; CUTOUT DMG IAW 53-10-08 FIG 202; HFEC INSPEC IAW B737 NTM PT.6 51-00-00 FIG 23 NO CRACKS NOTED; REPAIRED INTERCOSTAL WITH FILLER, ANGLE, AND RADIUS BLOCK; INSTALLED IAW SRM 53SDR AWXA0001049Skin · scratchedFUSELAGE SKIN STA 1060-1070 L14L HAS DEEP SCRATCH UNDER W OF TAIL NUMBER - FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN, NDT NO CRACKS NOTED; FABED REPAIR PLATE, INSTALLED REPAIR PLATE, INSTALLED CONICAL WASHERS IAW SRM 53-00-01, 51-40-02SDR AWXA0001048Bulkhead · crackedCENTER WEB CRACKED FS 178 WL 187 LBL 0.7 (1.9) AND RBL 0.7 (1.5L). REMOVED DAMAGED AREA, FABED AND INSTALLED REPAIR PARTS IAW SRM 53-10-08 FIG 203SDR AWXA0001047Bulkhead · crackedCENTER WEB CRACKED FS 178 RBL 5.0 WL 198 (1.3L) AND WL 202 (0.9L). REMOVED DAMAGE, FABED AND INSTALLED REPAIR PARTS IAW SRM 53-10-08 FIG 209SDR AWXA0001046Bulkhead · crackedCENTER WEB CRACKED FS 178 LBL 5.0 WL 198 & 202. REMOVED DAMAGE, FABED AND INSTALLED PARTS IAW SRM 53-10-08 FIG 209SDR AWXA0001050Frame · crackedCABIN RT I/B FWD OVERWING EXIT FRAME SUPPORT CRACKED AT BOTTOM FASTENER HOLE AREA STA 616 STR 17R BELOW CABIN FLOOR PANEL. REMOVED FASTENERS AND COLLARS, CUT OUT DAMAGE, NDT CUTOUT NO CRACKS NOTED, FABED AND INSTALLED REPAIR PARTS IAW ER-03-5310-00339-JS1 AND SDR AWXA0000881Adc · failedINBOUND TO ONT FAILURE FLAGS DISPLAYED ON CAPTAINS AIRSPEED IND, VMO POINTER, MACH ASI, ALTIMETER, VSI FAIL AND SPEED TAPE FAIL ON CAPT''S HORIZON GPWS ALSO FAILED. RESET ADC CIRCUIT BREAKER, RERACKED NR 1 AND 2 ADC, POWERED DOWN AND POWERED UP AIRCRAFT. ALLSDR AWXA0000492Blower · failedON DESCENT TO LGB, ACRID SMELL NOTED BY ALL CREW MEMBERS. MEL ISSUED. REMOVED AND REPLACED E & E BLOWER (NML POSITION) AND FLOW SENSOR, OPS CHECK NORMAL. NO HISTORY IN LAST 90 DAYS.SDR AWXA9900448Tie Clip · crackedSTRINGER CLIP CRACKED STR 15L STA 1040. REMOVED DAMAGED PART PER SRM 51-40-02, FABRICATED REPLACEMENT PART FROM 7075T6 .032 QQA 250/134 R682523 IAW SRM 51-30-01, TREATED AND PRIMED REPLACEMENT PART IAW 51-20-01. INSTALLED PART IAW SRM 51-40-02 RECOMMENDATIOSDR AWXA9900447Tie Clip · crackedREMOVED DAMAGED PART PER 737-300 SRM 51-40-02, FABRICATED REPLACEMENT PART FROM 7075T6 - .032 QQA250/13 R682523 IAW SRM 51-30-01 TREATED AND PRIMED PART IAW SRM 51-20-01. INSTALLED REPLACEMENT PART IAW SRM 51-40-02 RECOSDR AWXA9900446Skin · crackedL-1 DOOR JAMB AFT LWR CORNER HAS 1 CRACK .25 LONG COMING OUT OF FASTENER .125 INCH ON EACH SIDE OF FASTENER. REPAIRED L-1 DOOR JAMB AFT LWR CORNER FUSELAGE SKIN CRACKS PER ER 03-5330-99314-EY5. FABRICATED REPAIR FILLER USING MAT'L 2024T3 - .071 QQA250/5 R700SDR AWXA9900445Skin · crackedR-1 DOOR JAMB AFT LWR CORNER HAS 3 CRACKS, ALL START FROM EDGE TWO 1/4 CRACKS STOP AT FASTENERS ONE EXTENDS PAST FASTENER. CUT OUT DAMAGED AREA, ACCOMPLISHED HFEC. NO CRACKS NOTED. FABRICATED OUTER DOUBLER FROM .100 2024T3 - R641191 BOTH MIDDLE AND INNER DOSDR AWXA9900441Skin · crackedCRACK IN FUSELAGE SKIN AT THE UPPER CORNER OF L-2 DOOR HINGE CUTOUT. DAMAGED MATERIAL REMOVED, FABRICATED REPAIR DOUBLER OF 301 1/2 HARD 2660361 AND FILLER 2024-T3 .071 QQA250/5 R700681. INSTALLED REPAIR IAW 53-69-01.SDR AWXA9900442Frame · crackedUPPER PART OF FRAME 500 HAD A CRACK APPROXIMATELY 1.5 INCH LONG AT BL 0 IN THE FWD CARGO COMPARTMENT. STOP DRILLED CRACK, FABRICATED A REPAIR DOUBLER PER 737 SRM 53-00-07 FIG 201 OF QQA 250/13 T6 .05 R698980. TREATED, PRIMED AND INSTALLED IAW 737 SRM 53-0SDR AWXA9800196Charger · inoperativeEMERGENCY EXIT LIGHTS FROM ROW 19 TO 23 ON PAX SEATS INOP. REPLACED AFT BATTERY CHARGER, CHECK OK.SDR AWXA9700552Skin · dentedDURING ROUTINE MAINTENANCE CHECK, FOUND DENT AT BS 405 ABOVE STR 16L. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-00-01.SDR AWXA9700551Stringer · corrodedDURING ROUTINE MAINTENANCE CHECK, FOUND FUSELAGE STRINGER 16 RT AT WING SCANNING LIGHT CUTOUT TO BE CRACKED AT STA 500C + 4 AND 500C + 16. REPAIRED DAMAGED STRINGER 16 RT, STA 500C + 4 AND 500C + 16 IAW SB 737-53-1145 PER ER 3-53-14-08.SDR AWXA9700550Track · corrodedDURING ROUTINE MAINTENANCE CHECK, FOUND LEFT WING, OUTBOARD FOREFLAP, OUTBOARD TRACK HAS CORRODED HOLES. REMOVED AND REPLACED OUTBOARD TRACK OHM 20-50-01.SDR AWXA9700549Carriage · corrodedDURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON NR 7 MAIN CARRIAGE SPINDLE. REMOVED AND REPLACED NR 7 CARRIAGE PER MM 27-51-44.
Back to N165AW, cancelled May 20, 2002