Boeing 727-22C
Service difficulty reports · 2,328
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 = '72722C' 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 = '72722C' 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 RAAA97B2011Floor Link · corrodedDURING SCHEDULED S4 STRUCTURAL/CPCP INSPECTION PER CARD S4 14108, FOUND BS 740 SEAT TRACK FLOOR LINK ATTACH POINTS WORN AND UPPER FLANGES CORRODED AT LBL 45.5, BL 0, RBL 24.75 AND RBL 45.5. REPLACED FLOOR LINKS, SEAT TRACKS, BUSHINGS AND BOLTS PER SRM 51-10-1SDR RAAA97B2010Seat Track · corrodedDURING SCHEDULED S4 STRUCTURAL/CPCP INSPECTION PER CARD S4 14108, FOUND RBL 45.5 SEAT TRACK INBOARD CHORD LOWER SURFACE CORRODED AT BS 862. REPAIRED PER SRM 51-40-4 FIG 1.SDR RAAA97B2009Spar Chord · corrodedDURING SCHEDULED S4 STRUCTURAL/CPCP INSPECTION PER CARD S4 14108, FOUND CENTER WING UPPER REAR SPAR CHORD CORRODED, LBL 50 TO LBL 70 AND RBL 40 AT BS 870. REPLACED CENTER WING UPPER REAR SPAR CHORD PER BOEING MSG 9710012RR AND 970010TR.SDR RAAA97B2008Angle · damagedDURING SCHEDULED C1 CHECK, FOUND AFT CARGO COMPARTMENT FLOOR SUPPORT RBL 24 Z-ANGLE HOLED AT BS 1130 AND CORROSION BLENDOUT BEYOND LIMITS AT BS 1050. REPLACED Z-ANGLE FROM BS 1044 TO 1140 PER SRM 51-40-4 FIG 1, SHEET 5.SDR RAAA97B2007Stiffener · crackedDURING SCHEDULED C1 CHECK, FOUND NR 3 SPOILER OUTBOARD MOUNT STIFFENER ON REAR SPAR CRACKED AT WS 519. REPLACED STIFFENER PER SRM 51-30-02.SDR RAAA97B2006Frame · corrodedDURING AD 94-02-04 INSPECTION, FOUND LT BS 783.95 FRAME WEB CORRODED AT WL 200. REPAIRED PER S/B 727-53-197.SDR RAAA97B2005Fitting · corrodedDURING SCHEDULED C1 CHECK, FOUND LEFT AFT CENTER WING TERMINAL PIN FITTING CORRODED BETWEEN PREVIOUS REPAIR PLATES ON INBOARD FLANGE AT BS 870. REPAIRED PER S/B 727-53-27, DWG 65-82247 AND 65-78694.SDR RAAA97B2004Casting · crackedDURING SCHEDULED C1 CHECK, FOUND LMLG UPLOCK ASSEMBLY ATTACH CASTING CRACKED AT FORWARD LUG, BS 910. REPLACED CASTING PER S/B 727-53-103.SDR RAAA97B2003Link Assembly · crackedDURING SCHEDULED C1 CHECK, FOUND LMLG UPLOCK MOUNT ASSEMBLY OUTBOARD FORWARD LINK ASSY CRACKED AT BS 910. REPLACED PER SRM 51-10-1.SDR RAAA97B2002Seat Track · corrodedDURING SCHEDULED S4 STRUCTURAL/CPCP INSPECTION PER CARD S4 14106, FOUND BL 0 SEAT TRACK CORRODED FROM BS 1130 TO 1176. REPLACED AND SPLICED CENTER SEAT TRACK PER SRM 53-10-5.SDR RAAA97B2001Chord · crackedDURING AD 94-07-08 INSPECTION, FOUND RT LOWER TORQUE BOX UPPER CHORD CRACKED AT BS 1263. REPAIRED PER S/B 727-53-129 AND DWG NR 65-C-27136.SDR DHL9770522CRib · crackedAT C CHECK, RIGHT WING RIB UPPER CHORD AT BL 70.5 INSPECT PER S/B 57-0112. NDT INSPECTED, TWO CRACKS NOTED, STOP DRILLED CRACKS, HFEC, ACCOMPLISHED S/B 57-112. INSTALLED KIT COMMON TO RT WING JUST OUTBD AND COMMON TO CENTER TANK. INSTALLED REMAINDER OF REPSDR DHL9770518CDoor · crackedAT C CHECK, AFT CARGO DOOR HAS A CRACK IN UPPER AFT CORNER ON FRAME BETWEEN SKIN AND SEAL. STOPPED DRILL CRACK, HFEC, INSTALLED REPAIR PER AVITAS ENGIN DRAW 97PMSI149D-1 A. REPAIR 12 BY 2 BY 1.5, N/R 3877.SDR DHL9770523CBraces · crackedAT C CHECK, THREE ATTACH BRACES IN TAIL SKID COMPT CRACKED AT AFT END OF HORIZONTAL BRACES. REMOVED AND REPLACED RT UPPER AND LOWER AND LEFT LOWER HORIZONTAL BRACES, IN TAIL SKID COMPARTMENT PER SRM 51-10-1 PARA 4 AND SRM 51-30-2. N/R 3821.SDR DHL9770519CMount · crackedAT C CHECK, NR 6 LEADING EDGE FLAP ACTUATOR MOUNT IS CRACKED AT LOWER OUTBOARD CORNER. REMOVED ACTUATOR, REPLACED MOUNT ACTUATOR PER SRM 51-30-2. REINSTALLED ACTUATOR. N/R 2432.SDR DHL9770524CFitting · crackedAT C CHECK, COMPLY WITH PERMANENT REPAIR TO 940 FITTING CRACK. ACCESSED AREA, PER FORMED EDDY CURRENT INSPECTION OF FASTENER HOLES, INSTALLED NEW 940 FITTING PER S/B 53-0118. SEALED FASTENERS PER SRM 51-20-4. N/R 3663.SDR DHL9770521CTrunnion Fitting · crackedAT C CHECK, COMPLIED WITH PERMANENT REPAIR TO RIGHT HAND TRUNNION SUPORT FITTING AFT SIDE HAS 2 CRACKS. REMOVED NLG TRUNNION SUPPORT FITTING AS PER SRM 51-30-2. INSTALLED NEW SUPPORT FITTING PER DRAWING 65-88289, REINSTALLED NLG AND OPS CHECK PER M/M 32-21SDR DHL9770520CFitting · corrodedAT C CHECK, EVIDENCE OF CORROSION AT TIE FITTING BS 1183 AND STRINGER 20 LEFT. REPLACED TIE FITTING PER SRM 53-40-1 AND 51-30-2. N/R 3774.SDR DHL9770516CSeat Track · damagedDURING C CHECK, THE CENTER SEAT TRACK AT BL 0 WAS FOUND WITH BROKEN LOBE AT BS1130. CUTOUT DAMAGED SECTION OF SEAT TRACK AT BL 0, BS1166 TO 1120 PER SRM 53-10-5. INSTALLED NEW SEAT TRACK AT BL0 AS PER SRM 53-10-5 FIG 1. LENGTH OF TRACK REPLACED 55 1/2. NONSDR DHL9770515CFitting · corrodedDURING C CHECK, THE NOSE LANDING GEAR DRAG BRACE SUPPORT FITTING WAS FOUND TO HAVE HEAVY PITTED CORROSION AT LT SIDE ATTACHMENT AREA. REMOVED AND REPLACED NLG DRAG BRACE SUPPORT FITTING PER S/B 53-69. NON ROUTINE 3827.SDR DHL9770514CFrame · crackedDURING C CHECK, FRAME AT BS 1130 ABOVE STR 27LT WAS FOUND CRACKED AT SIDEWALL ATTACH ANGLE FASTENER. CUTOUT DAMAGED AREA AT BS 1130, FRAME UPPER FLANGE ABOVE STR 27 LT PER SRM 51-40-3. INSTALLED DOUBLER REPAIR PER SRM 51-40-3. SIZE OF REPAIR 7 BY 3. NON ROSDR DHL9770513CFrame · crackedDURING C CHECK, FRAME AT BS 1070 BETWEEN STR28RT AND 27RT WAS FOUND CRACKED. CUTOUT DAMAGED FRAME AT BS 1070 BETWEEN STR 28RT AND 27RT BELOW FLOOR SUPPORT Z ANGLE. INSTALLED REPAIR ON FRAME 1070 BETWEEN STR28RT AND 27RT AS PER SRM 51-40-3 PAGE 4. INSTALLED SDR DHL9770510CSkin · corrodedDURING C CHECK, NLG CUTOUT, AFT LT CORNER WAS FOUND TO HAVE SKIN BULGES AND DISHED FASTENERS AT BS 328. CUTOUT CORRODED AREA PER SRM 53-30-3. INSTALLED DOUBLER REPAIR AS PER SRM 53-30-3 AT NLG CUTOUT, AFT LT CORNER BS 328. REPAIR SIZE 15 BY 6. NON ROUTINE SDR DHL9770506CSkin · corrodedDURING C CHECK, BULGING WAS NOTED AT FUSELAGE SKIN STA 352.2 RT SIDE AFT OF NLG CUTOUT. CUTOUT BULGING SKIN AREA DUE TO CORROSION. INSTALLED EXTERNAL DOUBLER AT STA 352.2 RT SIDE AFT OF NLG CUTOUT AS PER SRM 53-30-3 FIG 1. SIZE OF REPAIR 13.5 BY 6.5. NON ROSDR DHL9770503CRib · crackedDURING C CHECK, THE NR 1 SLAT ON THE LEFT WING AT THE INBOARD TRACK HAS A CRACK IN RIB SECTION, AT THAT TRACK. STOP DRILLED CRACKS, ACCOMPLISHED HIGH FREQUENCY EDDY CURRENT INSP AND INSTALLED RIB REPAIRS INBOARD AND OUTBOARD PER SRM 57-50-3 FIG 9. SIZE OF RESDR DHL9770509CFitting · crackedDURING C CHECK, RIGHT SIDE BS 940 FRAME FITTING FOUND CRACKED AT UPPER ATTACH FLANGE THROUGH INBOARD FASTENER COMMON TO FITTING AND FLOORBEAM. TRIMMED OUT DAMAGED SECTION OF 940 FITTING AT FORWARD UPPER ATTACH FLANGE PER BOEING TELEX 32-9430. PERFORMED HFEC SDR DHL9770508CFitting · gougedDURING C CHECK, MAIN CARGO DOOR LOWER EDGE CAM LATCH SUPPORT FITTING AT BS 600 WAS FOUND GOUGED AND NICKED. REMOVED AND REPLACED CAM LATCH SUPPORT FITTING ON MAIN CARGO DOOR, LOWER EDGE AT BS 600 PER SRM 51-10-1 PAR 4 AND 51-31-2. NON ROUTINE 3736.SDR DHL9770504CFitting · crackedDURING C CHECK, THE NR 6 FLAP TRACK, FORWARD SIDE OF FALSE SPAR SUPPORT, FITTING INBOARD SIDE CRACKED AT WBL 203. REMOVED AND REPLACED FITTING PER 51-30-2. NON ROUTINE 2414.SDR DHL9770501CRib · crackedDURING C CHECK, A CRACK WAS FOUND IN THE RIB ON THE L/W AT WS 656 AT LOWER STR NR 2. STOP DRILLED CRACK AT BOTH ENDS AND INSTALLED RIB REPAIR AT LOWER SECTION OF RIB, STR NR 2, AS PER S/B 727- 57-127. NON ROUTINE NR 1226.SDR DHL9770517CFitting · crackedAT C CHECK, STRINGER TIE FITTING CRACKED AT STA 360 STRINGER 19RT. REPLACED TIE FITTING PER SRM 51-30-2. NR 3878.SDR DHL9770512CStringer · crackedDURING C CHECK, BULGING OF THE FUSELAGE SKIN WAS NOTED AT STR 25RT, AFT OF BS 1166. FOUND STRINGER 25 RT CRACKED. CUTOUT STRINGER FROM BS 1175 TO 1183. INSTALLED STRINGER REPAIR PER SRM 53-10-3. NON ROUTINE 3790.SDR DHL9770507CFitting · gougedDURING C CHECK, MAIN CARGO DOOR LOWER EDGE CAM LATCH SUPPORT FITTING AT STA 560 WAS FOUND GOUGED AND NICKED. REMOVED AND REPLACED LATCH SUPPORT FITTING AT LOWER EDGE OF THE MAIN CARGO DOOR STA 560 PER SRM 51-10-1 AND 51-30-2. NON ROUTINE 3734.SDR DHL9770505CRib · crackedDURING C CHECK, R/W INTERIOR WS 629.0 WING RIB LOWER FLANGE CRACKED AT STR 6. STOP DRILLED CRACK. PERFORMED HFEC CHECK. INSTALLED REPAIR PER SRM 57-10-5 PAGE 4 AT R/W WS 629, STR 6 PER S/B 727-57-127. REPAIR SIZE 3X8. NON ROUTINE 2476.SDR DHL9770502CRib · crackedDURING C CHECK, A CRACK WAS FOUND AT LEFT WS 686.5 LOWER FLANGE OF RIB AT STR 6 ATTACH POINT. STOP DRILLED CRACK AT BOTH ENDS. INSTALLED WING RIB REPAIR AT LT WING STA 686.5 PER SRM 57-10-5 PAGE 5. REPAIR SIZE 1X8X3. NON ROUTINE 1228.SDR DHL9770511CDoubler · misinstalledDURING C CHECK, DOUBLER INSTALLED AT STR 20LT BS 1130 WAS FOUND OUT OF CONFORMITY WITH BOEING SRM. REMOVED EXISTING DOUBLER AND INSTALLED DOUBLER REPAIR AT STR 20L, BS1130 LAP SEAM PER SRM 53-30-3 FIG 5. REPAIR SIZE 9.5 BY 8.5. NON ROUTINE 3789.SDR 97ZZZM696Clamp · brokenNR 3 ENGINE FIRE WARNING ON CLIMB. REPLACED BROKEN CLAMP ON BLEED AIR DUCT.SDR 97ZZZX1759Fitting · crackedINSPECTION FOUND 1.5 INCH CRACK AT BS 940 FRAME FITTING FORWARD UPPER ATTACHED FLANGE. SUSPECT CAUSE, FATIGUE.SDR RAAA97B1004Battery Pack · dischargedROW 10 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. REPLACED BATTERY PACK DUE DISCHARGED.SDR RAAA97B1003Battery Pack · dischargedROW 7 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. REPLACED BATTERY PACK DUE DISCHARGED.SDR RAAA97B1002Battery Pack · dischargedROW 2 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. REPLACED BATTERY PACK DUE DISCHARGED.SDR 97ZZZX2973Connector · looseNR 3 ENGINE FIRE WARNING ON CLIMB. TIGHTENED 8TH STAGE BLEED AIR DUCT CLAMP AND FIRE LOOP CONNECTOR. REF: OPERATOR CONTROL NR 97ZZZX2972. (X)SDR 97ZZZX2972Clamp · looseNR 3 ENGINE FIRE WARNING ON CLIMB. TIGHTENED 8TH STAGE BLEED AIR DUCT CLAMP AND FIRE LOOP CONNECTOR. REF: OPERATOR CONTROL NR 97ZZZX2973. (X)SDR UPS97222377Shut Off Valve · failedINSPECTION TYPE-N/A, SMOKE IN FLIGHT DECK. FOUND LEFT PACK SOV, FAILED OPEN AND PACK COOLING FAN CB PULLED DUE TO DI 126385. REMOVED AND REPLACED LEFT PACK SOV PER MM 21-51-61. REMOVED AND REPLACED LEFT ACM PER MM 21-51-11, PRECAUTIONARY. INSPECTED SYSTEMSDR RAAA97B1001Light · failedFORWARD RT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT STAYS ON DURING SERVICE CHECK. REPLACED EGRESS IDENTIFIER LIGHT ASSY.SDR DHL97705003Switch · failedON GEAR EXTENSION RT MAIN GREEN GEAR LIGHT WAS NOT ON AND GEAR DOOR LIGHT ON FWD PANEL WAS ON. ALL RED GEAR LIGHT WERE OUT, NO AMBER DOOR LIGHTS AT S/O PANEL. GEAR AOM CAME ON AT FLAPS 30Ý MECHANICAL RT GEAR INDICATOR WAS IN GREEN BAND. INSPECTED A/C, FOUND SDR DHL97705001Actuator · failedAFTER TAKEOFF, DURING FLAP RETRACTION, THE L/E FLAP AMBER LIGHT REMAINED ON, ON THE SECOND OFFICIER S-PANEL. THE LED ANNUNCIATOR LIGHT ON THE L/E NR 3 SLAT WAS ILLUMINATED. PERFORMED ALTERNATE PROCEDURE. REMOVED AND REPLACED ACTUATOR PER M/M.SDR 97FDEA00100Doubler · corrodedNR 0578 031, CORROSION (C53-221-01) ON COCKPIT FLOOR AND ON ATTACHED ANGLE AT BS 225, RBL 20 TO 26. *S/D* REMOVED CORROSION ON COCKPIT FLOOR AND ATTACHED ANGLE AT BS 225, RBL 20 TO 26 PER FED-EX SRM 51-10-6. FOUND TO BE OUT OF LIMITS IN VARIOUS AREAS PER FESDR 97FDEA00099Frame · corrodedNR 0633 030, CORROSION (53-221-01) AT FRAME STA 227 AFT O/B ANGLE, WL 235 RT. *S/D* REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. REMOVED, FABRICATED AND INSTALLED FRAME AT STA 227 AT WL 235 RT SIDE. ALL WORK ACCOMPLISHED PER FED-EX SDR 97FDEA00095Ceiling Support · corrodedNR 0357 028. CORROSION (C53-111-01) ON CENTER CEILING SUPPORT FROM BS 660 TO BS 500, WL 200 BL ZERO. REMOVED CORROSION FROM CEILING SUPPORT STABILIZER BS 500 TO 660, BL ZERO, WL 199 AND FOUND OUT OF LIMITS IN NUMEROUS AREAS PER FED-EX SRM 53-10-1. REMOVSDR 97FDEA00082Floorbeam · corrodedNR 0283 027. CORROSION C53-224-01(1) ON FLOORBEAM UPPER FLANGE BOTTOM FWD SIDE AT BS 360, LBL 56, WL 207.8. REPAIRED FLOORBEAM AT BS 360, LBL 56, WL 208. CORROSION FOUND TO BE OUT OF LIMITS. REPAIRED PER FED-EX SRM 53-10-8 FIG 8.
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