Boeing 727-243
Service difficulty reports · 534
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 = '727243' 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 = '727243' 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 GAIA02041STHinge · crackedDURING A CPCP INSPECTION, IT WAS DISCOVERED THAT THE MAIN CARGO DOOR AFT HINGE UPPER SECTION CRACKED AT THE LAST TWO LOBES, BS 650. REMOVED AND REPLACED MAIN CARGO DOOR HINGE.SDR CA020325008Duct · ruptured(CAN) NR 2 ENGINE FAILED ON TAKEOFF WITH AN AUTO PACK TRIP. AFTER ABORTED TAKEOFF THE A/C RETURNED TO THE GATE IN AND SUBSEQUENT INSPECTION REVEALED A RUPTURED 13TH STAGE SADDLE DUCT.NEW DUCT INSTALLED ENGINE GROUND RUN SATISFACTORY AND A/C RELEASED FOR SERVISDR GAIA02018STFrame · crackedDURING INSPECTION, IT WAS DISCOVERED THAT A FUSELAGE FRAME WAS CRACKED AT STATION 640. ACCOMPLISHED FRAME REPAIR IAW B727 SRM 51-40-3. (M)SDR GAIA02017STFrame · crackedDURING INSPECTION, IT WAS DISCOVERED THAT A FUSELAGE FRAME WAS CRACKED AT STATION 580. ACCOMPLISHED FRAME REPAIR IAW B727 SRM 51-40-3. (M)SDR EISA20010151Skin · tornACCOMPLISHED SHEET METAL REPAIR AREA FORWARD OF RT OUT FLOW VALVE, STA 1166, STR. 24R.CORRECTIVE ACTION:CUT OUT DAMAGED AREA. FABRICATED DOUBLER .071 2024-T3 8" X 12" IAW B727 SRM 53-30-3, FIG. 3. TREATED & PRIMED AND INSTALLED DOUBLER IAW B727 SRM 51-10-2 & SDR CA011219010Key · broken(CAN) DURING PUSH BACK NR 2 BRAKE LOCKED UP. NR 2 MAIN WHEEL AND BRAKE ASSY REPLACED. OVERHAUL SHOP FINDINGS AS FOLLOWS: BRAKE ASSY: PRIMARY CAUSE FOR REMOVAL FOD DAMAGE FROM WHEEL. MAIN WHEEL ASSY. PRIMARY CAUSE FOR REMOVAL BROKEN BRAKE KEYS.SDR CA011210015Key · broken(CAN) DURING PUSH BACK, NR 2 BRAKE LOCKED UP. NR 2 MAIN WHEEL INSIDE WHEEL RIM BRAKE KEYS FOUND BROKEN. NR 2 MAIN WHEEL ASSY AND NR 2 BRAKE ASSY. REPLACED. AWAITING OVERHAUL SHOP FINDINGS ON EACH COMPONENT FOR PROBABLE CAUSE.SDR GAIA01315OPLight · defectiveDURING ROUTINE MAINTENANCE AT FWA, IT WAS DISCOVERED THAT THE L1 EMERGENCY EXIT LIGHT WAS DIM. MAINTENANCE REPLACED THE EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR EISA20010119Structure · crackedRT HORIZONTAL STAB O/B T/E CORNER IS CRACKED, TOP SIDE. FOUND DURING B-CHECK. ROUTED OUT CRACK IAW B727 SRM 55-10-1. NDT VERIFIED CRACK BEING REMOVED. FABRICATED DOUBLER AND FILLER PER EO NR 01-236. INSTALLED REPAIR PER EO 01-236 & B727 SRM 57-30-2 WITH APPRSDR CA010628054Key · missing(CAN) ON SERVICE CHECK INSPECTION NR 2 MAIN GEAR BRAKE ASSY, PISTON HOUSING FOUND DAMAGED BEYOND LIMITS DUE TO NR 2 MAIN WHEEL ASSY. MISSING A BRAKE KEY. NR 2 MAIN GEAR BRAKE ASSY AND NR 2 MAIN WHEEL ASSY REPLACED IN ACCORDANCE WITH MAINTENANCE MANUAL. NO FURTSDR GAIA01153OPGuard · brokenDURING ROUTINE INSPECTION AT BOI, FOUND EMERGENCY EXIT LIGHT SWITCH GUARD BROKEN. REMOVED AND REPLACED SWITCH GUARD ON EMERGENCY EXIT LIGHT SWITCH. OPS CHECK NORMAL AT THIS TIME. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR CA010314006Circuit Board · shorted(CAN) ON TAKEOFF ROTATION MASTER WARNING LIGHT ILLUMINATED WITH NO LOSS OF ESSENTIAL POWER, ELEVATOR LOW PRESSURE LIGHT, GPWS WARNING LIGHTS, FLIGHT CONTROL PCU LIGHTS, ALL OIL PRESSURE/FILTER BYPASS LIGHTS, FLIGHT INSTRUMENT TRANSFER LIGHTS TRANSPONDER FAIL LSDR EISA20000196Plate · misalignedPACK FAN REMAINED ON AFTER FLAPS UP. RUDDER LOAD LIMITER LIGHT REMAINED ON FOR 4 MINUTES AFTER FLAPS UP. REMOVED AND REPLACED RIVETS ON STRIKER ON INBOARD FLAP CONTROL VALVE FOLLOW UP PULLEY. OPS CHECKED INBOARD FLAP FOLLOW UP CABLES, RUDDER LOAD LIMITER INSDR GAIA00515Switch · out of adjFLT 2035 - PDX-MHR - ON APPROACH, LE DEVICES AND OUTBOARD FLAPS WOULD NOT EXTEND. COMPLIED WITH CHECKLIST AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED AT MHR WITHOUT ANY FURTHER DIFFICULTIES. ADJUSTED FLAP UP SWITCH. CYCLED FLAPS UP AND DOWN. OPERATIONASDR GAIA00513Indicator · inoperativeFLT 2035 - PDX-MHR - ON APPROACH, LE DEVICES AND OUTBOARD FLAPS WOULD NOT EXTEND. REFERENCED PROCEDURES AND DECLARED AN EMERGENCY. TROUBLESHOT AND FOUND RIGHT OUTBOARD FLAP POSITION TRANSMITTER TO BE INTERMITTENT. INSTALLED NEW TRANSMITTER. RAN FLAPS SEVERSDR GAIA00488Indicator · failedFLT 2032 - MHR - ON FLAP RETRACTION OUTBOARD FLAPS READ 2 DEGREES, WHILE THE INBOARD FLAPS READ 5 DEGREES. AIRCRAFT MADE AN UNEVENTFUL RETURN TO MHR. EXTENDED FLAPS, INSPECTED ALL FLAPS, CLEANED AND LUBED ALL FLAP TRACKS AND JACK SCREWS. LUBED GIMBIES, CLEASDR GAIA00382Downlock Sensor · failedFLT 2015 - BIL-DEN - WHEN GEAR SELECTED DOWN. THE RIGHT GEAR UNSAFE LIGHT REMAINED ILLUMINATED, SHOWING RIGHT MAIN GEAR NOT EXTENDED. THE CREW CARRIED OUT EMERGENCY PROCEDURES. THE AIRCRAFT MADE A SAFE LANDING WITH NO FURTHER PROBLEMS. MAINTENANCE TROUBLE SDR GAIA00208Firewall · crackedDURING ZERO B-CHECK AT STAMBAUGH/BQK, FOUND NR 1 ENGINE PYLON FIREWALL CRACKED OUT AT NAC STATION 146. REPAIRED IAW SRM 54-10-0 AND BOEING REPAIR SKETCH STS-BQK-99-00003H/00005H. REPAIR CARRIED OUT ON STS WORK ORDER SROO522, NR0018. AIRCRAFT RETURNED TO SERSDR GAIA00209Stringer · corrodedDURING ZERO B-CHECK AT STAMBAUGH/BQK, FOUND IG CORROSION ON OUTBOARD FLANGE OF STRINGER 29L FORWARD OF PREVIOUS REPAIR AT STATION 950E (KEEL BEAM EXTENSION). REPAIRED IAW BOEING REPAIR SKETCH STS-BQK-99-00007H REPAIR CARRIED OUT OUT ON STS WORK ORDER SROO521,SDR GAIA00210Frame · crackedDURING ZERO B-CHECK AT STAMBAUGH/BQK, FOUND RIGHT STATION 580 AND STATION 600 FRAMES CRACKED APPROX 4 INCHES ABOVE MAIN CARGO DECK FLOOR LINE ON INBOARD FLANGE. REPAIRED IAW SRM 53-10-1. REPAIR CARRIED OTU ON STS WORK ORDER SROO521, NR0103. AIRCRAFT WAS RETSDR GAIA00211Frame · crackedDURING ZERO B-CHECK AT STAMBAUGH/BQK, FOUND RIGHT STATION 640 FRAME CRACKED APPROX 4 INCHES ABOVE MAIN CARGO DECK FLOOR LINE ON INBOARD FLANGE. REPAIRED IAW SRM 53-10-1 REPAIR CARRIED OUT ON STS WORK ORDER SROO521, NR0107. AIRCRAFT WAS RETURNED TO SERVICE. SDR GAIA00212Threshold · corrodedDURING ZERO B-CHECK AT STAMBAUGH/BQK, FOUND AFT LOWER CARGO DOOR THRESHOLD HAS CORROSION IN NUMEROUS AREAS AT FRAME. REPAIRED IAW BOEING REPAIR SKETCH STS-BQK-99-00008H. REPAIR CARRIED OTU ON STS WORK ORDER SROO521, NR0115. AIRCRAFT WAS RETURNED TO SERVICE.SDR GAIA00213Frame · corrodedDURING ZERO B-CHECK AT SAMBAUGH/BQK, FOUND IG CORROSION AT STRINGER 26L ON FORWARD WEB AND SKIN ATTACH LEG OF STATION 1148 FRAME. REPAIRED IAW SRM 53-10-4. REPAIR CARRIED OUT ON STS WORK ORDER SROO521, NR0138. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA00169Light · inoperativeDURNG PREFLIGHT AT FWA, IT WAS DISCOVERED DURING PREFLIGHT THAT THE EMERGENCY EXIT LIGHT WAS INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR GAIA00112Light · inoperativeDURING PREFLIGHT, UPON EMERGENCY EXIT LIGHT TEST, LIGHT DID NOT ILLUMINATE WHEN SWITCH MOVED TO ON POSITION (COCKPIT OVERHEAD PANEL) BUT DID COME ON WHEN TURNED ON AT THE LIGHT OVER COCKPIT DOOR. MAINTENANCE REPLACED FLIGHT DECK OVERHEAD DOOR EMERGENCY LIGHT SDR GAIA00109Warning Light · illuminatedFLT 1844 - FWA-ORF - DURING TAKEOFF, THE NR 2 ENGINE FIRE WARNING LIGHT ILLUMINATED AND BELL SOUNDED. THE CREW DECLARED A EMERGENCY LANDING BACK AT FWA. THE CREW RAN EMERGENCY CHECKLIST AND DISCHARGED FIRE BOTTLE. DURING SHUT DOWN NR 2 ENGINE, THROTTLE DIFFSDR GAIA00047Light · inoperativeDURING ROUTINE MAINTENANCE, FOUND EMERGENCY EXIT LIGHT OVER L-1 DOOR INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)SDR GAIA0012Seat Track · damagedDURING PHASE-IN INSPECTION, DAMAGE WAS FOUND ALONG CABIN SEAT TRACK FROM BS 950 TO 1135 RIGHT BODY LINE 25. REPLACED SECTION OF CABIN SEAT TRACK FROM BS 950 TO 1135, RBL 25. MATERIAL USED, PART NR CAB1520-792, 185 INCH LONG. REPAIR ACCOMPLISHED IAW SRM 53-1SDR GAIA0011Floorbeam · damagedDURING PHASE-IN INSPECTION, DAMAGE WAS FOUND ALONG CABIN FLOORBEAM SUPPORT BS 400, RIGHT BODY LINE 55. INSTALLED REPAIR AT CABIN FLOORBEAM SUPPORT BS 400, RBL 55. MATERIAL USED, PART NR BAC1505-100617 AND BAC1490-2831, T-ANGLE 15 INCH LONG, SUPPORT ANGLES, 1SDR GAIA0010Gusset · damagedDURING PHASE-IN INSPECTION, DAMAGE WAS FOUND ON GUSSET AT STATION 825 LEFT INNER FLANGE, LEFT BODY LINE. REPLACED GUSSET AT STATION 825 LEFT INNER FLANGE JUST ABOVE CENTER SECTION UPPER SKIN, LBL 70. MATERIAL USED, 7075-T6, .090 INCH, 5 INCH BY 3 INCH. REPASDR GAIA0009Floorbeam · damagedDURING PHASE-IN INSPECTION, DAMAGE WAS FOUND ALONG FLOORBEAM UPPER T-CAP AT STATION 344 LEFT BODY LINE 62.5 TO RT BODY LINE 62.5. REPLACED FLOORBEAM UPPER T-CAP AT STATION 344, LBL 62.5. MATERIAL USED, PART NR BAC1505-29222. REPAIR ACCOMPLISHED IAW SRM 53-1SDR GAIA0008Seat Track · damagedDURING PHASE-IN INSPECTION, DAMAGE WAS FOUND ALONG CABIN SEAT TRACK FROM BS 1080 TO 1135, RIGHT BODY LINE 45. REPLACED SECTION OF CABIN SEAT TRACK FROM BS 1080 TO BS 1135, RBL 45 IAW SRM 53-10-5 FIG 7. MATERIAL USED, PART NR BAC1520-792, 55 INCHES LONG. SEESDR GAIA0007Seat Track · damagedDURING PHASE-IN INSPECTION, DAMAGE WAS FOUND ALONG SEAT TRACK FROM STATION 344 TO 480 RIGHT BODY LINE 45.5. REPLACED SEAT TRACK FROM STATION 344 TO STATION 480, RBL 45.5. MATERIAL USED, PART NR CAB1520-792. ACCOMPLISHED IAW SUPPLEMENTAL TYPE CERTIFICATE (STSDR GAIA0006Seat Track · damagedDURING PHASE IN INSPECTION, DAMAGE WAS FOUND ALONG SEAT TRACK FROM STATION 344 TO 480, RIGHT BODY LINE 24.75. REPLACED SEAT TRACK FROM STATION 344 TO STATION 480, RBL 24.75. MATERIAL USED, PART NR CAB1520-792. ACCOMPLISHED IAW SUPPLEMENTAL TYPE CERTIFICATE SDR GAIA0005Seat Track · damagedDURING PHASE-IN INSPECTION, DAMAGE WAS FOUND ALONG SEAT TRACK FROM STATION 344 TO 480 LEFT BODY LINE 45.5. REPLACED SEAT TRACK FROM STATION 344 TO STATION 480, LBL 45.5. MATERIAL USED, PART NR BAC1520-792. ACCOMPLISHED IAW SUPPLEMENTAL TYPE CERTIFICATE (STCSDR EISA2000001Receiver · shortedNR 1 NAV RECEIVER INOPERATIVE. INSTALLED SERVICEABLE NAV RECEIVER. (M)SDR CALA9901738Battery Pack · dischargedINSPECTION FOUND SEVERAL EMERGENCY LIGHTS INOPERATIVE IN CABIN AND AT OVERWING EXITS, BOTH SIDES. MAINTENANCE REPLACED A BAD FUSE. THE BATTERY PACKS WERE REMOVED, RECHARGED, AND REINSTALLED. OPERATIONAL CHECKS WERE GOOD IAW MM 33-50-01, PAGE 201.SDR CALA9900928Floorbeam · corrodedINSPECTION FOUND FORWARD LAV FLOORBEAM CORRODED AT STA 327, RBL 44-60. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03889.SDR CALA9900418Skin · corrodedINSPECTION FOUND AFT LAV SERVICE PANEL AFT LOWER SKIN CORRODED. THE PANEL WAS REMOVED AND THE CORRODED INNER SKIN WAS REMOVED. A NEW SKIN AND INTERNAL AND OUTER DOUBLER WERE INSTALLED AND THE PANEL WAS REINSTALLED IAW SRM 51-10-2, PAGE 1, 51-30-2, PAGE 1 ANDSDR CALA9900417Stringer · crackedINSPECTION FOUND A 4 INCH CRACK IN STRINGER 23L BETWEEN STA 1183 AND 1161, JUST BELOW LAV SERVICE PANEL INSIDE AFT CARGO COMPARTMENT. THE CRACKED SECTION OF STRINGER WAS CUT OUT, A NEW STRINGER, DOUBLER AND FILLER COVER PLATE WERE INSTALLED IAW SRM 51-10-2 ANSDR CALA9900407Skin · crackedINSPECTION FOUND A .5 AND .375 INCH CRACK IN LT O/B AILERON LOWER SKIN WITH A BEND AT I/B EDGE. THE AILERON WAS REMOVED AND REPLACED IAW MM 27-10-31.SDR CALA9900401Wire · brokenTHE RT FORWARD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE. THE WIRE WAS REPAIRED IAW WPM 20-10-13, PAGE 1. OPERATION OF THE EXIT LIGHT CHECKED GOOD.SDR CALA9900400Angle · crackedINSPECTION FOUND A 2.75 INCH CRACK IN LT WING REAR SPAR O/B SUPPORT ANGLE WHERE NR 2 SPOILER ACTUATOR AND FLAP DRIVE CASTING MOUNTS. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-2.SDR CALA9900398Bracket · crackedINSPECTION FOUND A .125 INCH CRACK AT UPPER END OF OUTBOARD BRACKET AT RT WING LEADING EDGE WHERE NR 5 L/E FLAP ACTUATOR MOUNTS. THE FASTENERS AND SUPPORT BRACKET WERE REMOVED IAW SRM 51-20-2. A NEW SUPPORT BRACKET WAS INSTALLED IAW SRM 51-10-1, PARAGRAPH 4 SDR CALA9900397Skin · debondedINSPECTION FOUND LT WING I/B MIDFLAP I/B END OF TRAILING EDGE SKIN DEBONDED. THE DEBONDED AREA WAS CUT OUT, A SKIN AND DOUBLER HOT BOND REPAIR WAS PERFORMED IAW SRM 51-40-6.SDR CALA9900396Control Tab · dentedINSPECTION FOUND THE RT ELEVATOR CONTROL TAB UPPER O/B TRAILING EDGE SKIN DENTED. THE ELEVATOR TAB WAS REMOVED AND REPLACED IAW MM 27-30-11.SDR CALA9900387Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN LT O/B FOREFLAP I/B END CASTING AT LEADING EDGE AND TRAILING EDGE. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-11.SDR CALA9900386Skin · debondedINSPECTION FOUND LT I/B FOREFLAP UPPER SURFACE DEBONDED. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-14.SDR CALA9900385Skin · debondedINSPECTION FOUND RT WING UPPER AND LOWER SKIN DEBONDED O/B AND AFT OF APU EXHAUST AREA. THE SKIN PANEL WAS REPAIRED IAW SRM 51-30-08 PAGE 1.SDR CALA9900384Skin · crackedINSPECTION FOUND A .3125 INCH CRACK IN RT INBOARD AFT FLAP LOWER LEADING EDGE. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-51-02.
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