Boeing 757-24APF
Service difficulty reports · 16,067
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 = '75724APF' 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 = '75724APF' 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 UPS07549076Frame · dentedINSPECTION TYPE:C AFT PIT RIGHT SIDE STA 1260 BETWEEN STR 25-26 FRAME DENTED. COMPLIED WITH EA 757-5362-27-A1567 AND UPS EO B757-5310-26027-A.SDR UPS07549050Frame · dentedINSPECTION TYPE:C - FOUND AFT PIT STA 1240, STR 2526 FRAME DENTED, RIGHT SIDE DIMENSION OF DENT .020 FROM CENTER OF DENT TO TRANS PANEL 5"4 FROM CENTER OF DENT TO PRODUCTIONS SPLICE 9.8 LENGTH OF DENT .900 W= 1.0. TRIMMED OUT DENTED AREA PER EA NR 757-53SDR UPS07548841Bleed Valve · odorBURNING SMELL DETECTED DURING FLIGHT AFTER R ENG BLEED VAL DISPLAYED, FOLLOWED FIM 36-10-00 FIG 110. REPLACED RT ENG HPSOV PER MM 36-11-07. OK TO CONTINUE.SDR UPS07548823Gcu · failedINSPECTION TYPE:N/A A/C DIVERTED TO MCO DUE TO RIGHT AC BUS FAILURE IN FLT. REMOVED AND REPLACED RIGHT ENG IDG PER MM 24-11-01-4. REMOVED AND REPLACED RIGHT ENG GEN CONTROL UNIT PER MM 24-22-02-4. REMOVED AND REPLACED BPCU PER MM 24-41-03-4. SYS OPS CHECKESDR UPS07548821Trunnion · bentNLG OPERATING SEQUENCE SLIDE ROD & TRUNNION ASSY BENT. A/C FERRIED TO MAE FOR REPAIR. REPLACED ROD ASSY & R&R TRUNNION ASSY IAW MM 32-34-06.NR930536 REPLACED SUPPORT ASSY IAW MM 32-34-06. PERFORM NLG EXTEMSION/RETRACTION TEST IAW MM 32-34-00 TEST GOOD. REPLASDR UPS07548812Hose · burstINSPECTION TYPE:N/A LEFT HYD QTY DECREASED TO ZERO & SYSTEM PRESS LIGHT ILLUM. EICAS MSG L HYD SYS PRESS DISPLAYED. INSPECTED LEFT MLG, FOUND DOWNLOCK ACT EXTEND HOSE BURST. REMOVED AND REPLACED EXTEND HOSE IAW B757 AMM 32-32-02. DUE TO EDP OPS W/O FLUID, SDR UPS06548757Unknown · fumesTOP OF DESCENT DESCENDING THRU VISIBLE MOISTURE SELECTED ENGINE ANTI-ICE STRONG FUMES IN THE COCKPIT. L PACK OFF R PACK ON, NO SMOKE VISIBLE. EMERGENCY DECLARED. RAN ENGINE FOR OVER 30 MIN, RAN PACKS, RAN ENGINE ANTI-ICE NO FUMES OR ODORS NOTED IAW M/M 21-00SDR UPS06548750Grommet · looseONE EMERGENCY ESCAPE DESCENT DEVICE HAS LOOSE RUBBER GROMMET DEVICE REMOVED FROM SLOT. REMOVED AND REPLACED EMERGENCY ESCAPE DESCENT DEVICE.SDR UPS06548751Warning Light · inoperativeEMERGENCY LIGHT UNARMED WARNING LIGHT INOP. RELAMPED, CK GOOD.SDR UPS06548749Switch · failedATB - EICAS DISPLAYED L HYD ELEC PUMP IN CLB, TROUBLESHOT TO LEFT PRESSURE SWITCH PER FIM. REMOVED AND REPLACED LEFT HYDRAULIC PRESSURE SWITCH IN REFERENCE TO MM 29-11-18-4. NO LEAK NOTED OK FOR SERVICE.SDR UPS06548739Pressure Switch · failedINSPECTION TYPE:N/A ATB - AFTER DEPARTURE THE CREW EXPERIENCED A HYD SYS PUMP FAILURE. THE A/C RETURNED TO SDF. NO EMERGENCY WAS DECLARED, AND THE A/C LANDED WITHOUT FURTHER INCIDENT. TROUBLESHOT THE LEFT PRESSURE SWITCH PER FIM. REMOVED & REPLACED LEFT HYSDR UPS06548731Light · inoperativeINSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS OFF, LIGHT NEXT TO SWITCH IS INOP, DOES NOT ILLUMINATE IN TEST MODE. RELAMPED, OPS CKS NORMAL PER MM 33-10-01.SDR UPS06548733Drive Assy · leakingPILOT REPORTED RIGHT ENGINE OIL LOSS ON DESCENT. INSPECTED NR 2 ENG. FOUND OIL LEAK COMING FROM THE HIGH SPEED GEARBOX RADIAL DRIVE. ACCOMPLISHED HS GEARBOX RADIAL DRIVE SHAFT SEAL REPLACEMENT IAW AMM 72-62-01-4. SERVICED ENGINE WITH OIL. ACCOMPLISHED ENGINE SDR UPS06548618Unknown · unknownINSPECTION TYPE:N/A ATB - LOW FUEL LIGHT ILLUMINATED IN FLIGHT. A 3000 LBS FUEL IMBALANCE BETWEEN LEFT 10.9, AND RIGHT 13.5 AFTER LANDING. NO DISCREPANCY NOTED PER FIM 28-41-00. PROCESSOR CH 1 AND CH 2 NO FAULTS, VERIFIED WITH NO FAULTS. OPS CHECK NORMAL. SDR UPS06548687Bulkhead · chafedINSPECTION TYPE:SIP NR 2 PYLON AFT BULKHEAD LT LOWER, OUTBOARDD CORNER CHAFED. MECH REQ. BULKHEAD MIL & NDT WERE DONE REF TRAV T6/641814. FILLER PLATE WAS FABBED ON TRAV T6/641938, GUSSETS WAS FABBED ON TRAV T6/641940. TREATED AND PRIMED GUSSETS, TREATED ASDR UPS06548686Bulkhead · chafedINSPECTION TYPE:SIP NR 1 PYLON AFT BULKHEAD LT LOWER, OUTBOARD CORNER CHAFED. MECH REQ. BULKHEAD MIL & NDT WERE DONE TRAV T6/641813, GUSSETS WERE FABBED REF TRV T6/6411937, FILLER WAS FABBED REF T6/641939. LOCATED AND DRILLED GUSSETS AND FILLER, TREATED ANDSDR UPS06548339Anti-Ice Valve · inoperativeDIVERSION, RT ENGINE ICE MESSAGE DISPLAYED WITH SWITCH ON. REMOVED AND REPLACED RT ENGINE INLET THERMAL ANTI-ICE VALVE IAW MM 30-21-03-4. OPS CHECK NORMAL.SDR UPS06548283Flex Line · leakingINSPECTION TYPE:N/A EMERGENCY DECLARED - LOSS OF BRAKING. CREW RECEIVED L HYD SYS PRESS MESSAGE. UPON TOUCHDOWN, APPLIED BRAKES WITH NO RESPONSE FROM BRAKE SYSTEM. PERFORMED 2 GO-AROUNDS. A/C LANDED SAFELY WITH NO FURTHER INCIDENT. (LEAKING FLEX LINE IN WSDR UPS06548530Bulkhead · chafedINSPECTION TYPE:C NR 2 PYLON AFT BULKHEAD RT OUTBD LOWER IS CHAFED. BULKHEAD MIL AND NDT WERE DONE ON TRAV NR T6/637434. GUSSETS WERE FABED REF NR T6/637410, FILLERS WERE FABED REF TRAV NR T6/637432 SHOT PEENED REWORKED AREA PER SOPM 20-10-03. FINISHED REPASDR UPS06548532Bulkhead · chafedINSPECTION TYPE:C NR 1 PYLON AFT BULKHEAD LT/OUTBD LOWER CHAFED. BULKHEAD MILL AND NDT WERE DONE REF TRAV NR T6/637465 GUSSETS WERE FABED REF TRAV NR T6/637463, FILLERS WERE FABED REF TRAV NR T6/637464. SHOT PEENED REWORKED AREA PER SOPM 20-10-03. INSTALLEDSDR UPS06548264Skin · damagedFOUND DAMAGE TO AIRCRAFT BELLY. REPLACED MAST ASSY & DRAIN HOSE, OPS CHKD NORMAL AS PER MM38-30-00 & 30-60-00. REPLACED 193AL PNL PER MM 53-30-00. CONDITIONAL CHECK NORMAL. A/C OK FOR SVC. HOSE P/N ON & OFF 79235-002 SN OFF NF516 THERMO P/N ON & OFF 3100-10SDR UPS06548247Skin Panel · damagedINSPECTION TYPE: DROP AFT FUSELAGE LWR SKIN DENTS BETWEEN STA 1589 AND 1614 REQUIRE REPAIR EA 757-5361-27-A14566. REPAIRS ACCOMPLISHED EA NR 757-5361-27-A14566 AND UPS EO NR B757-5330-25350-A, WITH NO DEVIATIONS.SDR UPS06548214Lock Actuator · warning messageINSPECTION TYPE:N/A ATB - GEAR DISAGREE MSG . SELECTED VMO/MMO SWITCH BACK TO NORMAL POS & SECURED. R&R NOSE GEAR LOCK ACTUATOR IAW B757 AMM 32-34-02-4, NO LEAKS NOTED. NOSE GEAR SYSTEM OPS CKS NORMAL IAW B757 AMM 32-34-00-5.SDR UPS06548246Skin Panel · damagedINSPECTION TYPE: DROP FUSELAGE DAMAGED AT BS 1500 TO 1540, S25R - 26R DUE TO CONTACT WITH GROUND EQUIPMENT. FUSELAGE REPAIR ACCOMPLISHED IAW EA NR 757-5361-27-A1558, AND UPS EO NR B757-5330-253479-A, WITH NO DEVIATIONS.SDR UPS06548203Engine · vibrationAT FL370 HAD IND OF HI N1 VIBRATION ON NR 1 ENG 2.6 VIB IND. DESCENDED TO FL260. IND'S WERE IN NORMAL RANGE AT THIS ALT DIVERSION WAS DETERMINED TO BE BEST COURSE OF ACTION.SDR UPS06548213Skin · tornCARGO CONTAINER STRUCK LOWER AFT AREA OF FUSELAGE JUST AFT OF REAR CARGO PIT. INTERIM REPAIR TO SKIN BTWN STA 1520 AND 1535 TRANSFERRED TO DFRL LIST. A/C FERRIED TO MAE FOR REPAIR. REF EO B757-5310-25284A.SDR UPS06548444Frame · dentedINSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1340, S26L DIMENSIONS OF THE DENT, 1.3'L BY 1.0'W BY 0.030' D REMOVE TRANSITIONAL PANEL LT STA 1310-1410 IAW SRM 51-40-02 TRIM OUT DENT AREA IAW EA 75 7-5362-27-A1561 STEP 1 PREM. TRIM OUT SIZE: 1.3' L BYSDR UPS06548447Frame · dentedINSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1340, S26R. TRIMMED OUT THE DENT AREA PER EA NR 757-5362-27-A1555 L=1", W= 1.0" D= .045". HFEC INSP PER EA NR 757-5362-27-A1555 STEP 2 OF DAMAGE REMOVAL INSP. NO NOTED CRACKS.SDR UPS06548178Engine · stalledAIR TURN BACK, LT ENG. EXPERIENCED APPROX. 5 COMPRESSOR STALLS IN APPROX 5 SECONDS. PASSING 1,300 FT. SHORTLY AFTER SELECTING V-NAV S SWITCHING FROM T/O TO CLB THRUST. EGT OVERTEMPED (RED) WENT TO 907 PEAK TEMP. ENGINE STABILIZED AND OPERATED NORMALLY WITH THRSDR UPS06548281Bulkhead · chafedINSPECTION TYPE:C NR 2 PYLON AFT BULKHEAD LT & RT LOWER CORNERS ARE CHAFED. BULKHEAD MILL & NDT WERE DONE ON TRAV T6/634336, GUSSETS WERE FABBED REF TRAV T6/635147, FILLERS WERE FABBED REF TRAV T6/635146. SHOT PEEN PER SOPM 20-10-03. INSTALLED REPAIR FILLERSDR UPS06548280Bulkhead · chafedINSPECTION TYPE:C NR 1 PYLON AFT BULKHEAD LT & RT LOWER CORNER CHAFED. BULKHEAD MILL AND NDT WERE DONE ON REF TRAV T6/634335 GUSSETS WERE FABBED REF TRAV T6/635145, FILLERS WERE FABBED REF TRAV T6/635144. S SHOT PEEN PER SOPM 20-10-03. INSTALLED REPAIR FILLSDR UPS06548170Engine · stalledLEFT ENGINE ON T/O STALLED AND EGT LIMIT WENT TO AROUND 855C FOR 7 SECS. ATB WAS ACCOMPLISHED. ACCOMPLISHED ALL STEPS OF POWERPLANT INSP AFTER A SURGE PER MM 71- 32-00/101 FIG 103. REMOVED AND REPLACED BVCU REF LP 532320, I2 AND TPCU REF LP 542316, I2. ACCSDR UPS06548279Frame · chafedINSPECTION TYPE:C MAIN CARGO DECK FUSELAGE FRAME AT STA 385 LT SIDE HAS CHAFE BETWEEN S STRINGERS 15-16 DAMAGE DIM. L= 0.104 W= 0.126 D= 0.045, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07-1A FIG 101 DETAILS I II IV PER EO B757-5310-20559-B. REPAIRED FRAME SDR UPS06548278Frame · dentedINSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1340, S26R. CUT OUT DAMAGED SECTION STA 1340 RT S=26R. L=.95" X W=1.0". HFEC IAW NTM 51-00-00, NO CRACK INDICATIONS NOTED COMPLIED WITH EA 757-5362-27-A1548 & UPS EO B757-5310-25385A.SDR UPS06548277Frame · dentedINSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1300, S26R. REMOVED TRANS PNL, CUT OUT DAMAGE S=26R L=.95 X W1.10. HFEC IAW NTM 51-00-00 PT 6, NO CRACK INDICATIONS NOTED REPAIRED IAW EA 757-5362-27-A1547, UPS EO B757-5310-25366.SDR UPS06548276Frame · dentedINSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1240, BETWEEN S26R - S27R. TRIMMED OUT FUSELAGE FRAME STA 1240 BETWEEN S26R-S27R. DAMAGE 0.790"L X .0950"W. HFEC IAW NTM 51-00-00, NO CRACK INDICATION NOTED. ENLARGED TRIM OUT BY 0.04" NEW DIM. L=0.830SDR UPS06548275Frame · dentedINSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1300, S26L. REMOVED TRANS PNL STA 1200-1300 LT SIDE FOR ACCESS, CUT OUT DAMAGE SECT. L=1.25" W=1.0". REMOVED TIE DOWN FITTING HFEC IAW NTM 51-00-PL 6, NO CRACK INDICATIONS NOTED COMPLIED WITH EA 757-5362SDR UPS06548271Frame · chafedINSPECTION TYPE:C MAIN CARGO DECK FRAME AT STA 365 HAS CHAFE BETWEEN STR 15R-16R. PERFORMED PARTIAL BLEND OF AREA OF FRAME DIMENSIONS ARE AS FOLLOWS: L= .6, W= .6, D= .013, ORIGINAL DAMAGE STILL EVIDENT. REPAIR ACCOM ON EA 757-5332-27-A1557 AND UPS EO B757-5SDR UPS06548270Frame · dentedINSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1280, S25L. TRIMMED OUT FUSELAGE STA 1280 FLANGE DAMAGED PER EA 757-5362-27-A1550, STEP NR 1 DIMENSIONS ARE 0.590"L X 0.900"W. HFEC IAW NTM 51-00-00 PT 6 NO CRACK INDICATIONS NOTED. COMPLIED WITH FINAL SDR UPS06547996A/C Pack · odorINSPECTION TYPE: N/A ON T/O AFTER SELECTING LT PACK OFF RT PACK PRODUCED BURNING SMELL THEN SUBSIDED IN THE CLIMB, SWITCHED PACKS. OK UPON LOG RT PACK PRODUCED THE SAME SMELL. UPON T/S SMELL NOTED AND RT PACK BITE MSG DISPLAYED WITH RT PACK OFF UPPER EICAS SCSDR UPS06548093Bulkhead · chafedINSPECTION TYPE:C ON NR 2 PYLON, AFT BULKHEAD RT SIDE LOWER CORNER GOUGED BLKHD MILL AND NDT WERE DONE ON TRAV #T6/628543. GUSSET WAS FAB ON TR AV #T6/630053, FILLER WAS FAB ON TRAV #T6/630052. SHOT PEEN REWORKED AREA PER SOPM 20-10-03. LOCATED AND DRILLED SDR UPS06548091Bulkhead · chafedINSPECTION TYPE:C NR 1 PYLON AFT BULKHEAD OUTBD LOWER LT AND RT CORNERS CHAFED BULKHEAD MILL AND NDT WERE DONE ON TRAV# T6/628660. GUSSETS WAS FABED ON TRAV NR T6/630051. FILLERS WERE FABED ON TRAV #T6/630060. SHOT PEEN REWORKED AREA PER SOPM 20-10-05. LOCSDR UPS06547970Light · inoperativeENTRY EMERGENCY LIGHT AT CREW DOOR INOP. REPLACED LAMP.SDR UPS06548158Frame · dentedINSPECTION TYPE:C DENT ON FRAME AT STA 1340 BET S26-L TO 27L. TRIMMED OUT DAMAGE AREA IAW EA 757-5362-27-A1536 PREM 1. INSTALLED REPAIR ANGLE IAW 757-5362-27-1535 PREM 2 ACCOMPLISHED FRAME REPAIR IAW EA757-5362-27-A1535.SDR UPS06548100Frame · dentedINSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1240 BET S25R TO S26R. TRIMMED OUT DAMAGE AREA IAW EA NR 757-5362-27-A1536 PREM 1 STEP 2 FINAL CUTOUT SIZE:1.140" L BY 1.240"W INSTALLED REPAIR ANGLE IAW EA 757-5362-27-A1536 STEP 10 AND 11 FINAL DIMENSIOSDR UPS06547944Inlet · obstructedHOT OIL SMELL IN COCKPIT, SEEMS TO BE ASSOCIATED WITH A PACK, POSSIBLY LEFT, BUT HARD TO SAY. NO OTHER INDICATION. LEFT PRE-COOLER OUT TEMP INDICATES 180 DEG. INSPECTED HEAT EXCHANGER INLET AND REMOVED BIRD'S NEST DEBRIS. PRE-COOLER OUT TEMP NOW READS 79 DSDR UPS06548031Frame · chafedINSPECTION TYPE:C FUSELAGE FRAME AT STA 1020, S15L HAS CHAFE DAMAGE NEAR FRAME RADIUS CUT AND TRIMMED DAMAGED AREA IAW SRM 51-70-12 FIGURE 1. PERFORM HFEC NO CRACKS NOTED. FABBED REPAIR ANGLES AND FILLER/SHIM. TREATED/PRIMED STRINGER CLIPS. INSTALLED ALL RSDR UPS06548032Frame · chafedINSPECTION TYPE:C FUSELAGE FRAME AT STA 940, S15L HAS CHAFE DAMAGE NEAR FRAME RADIUS. REMOVED 15 FASTENERS FROM FRAME STA 940 LT S15L -S16L FOR ACCESS IAW SRM 51-40-02. CUT OUT DAMAGE AREA IAW SRM 51-70-12-06. DIMENSIONS OF CUTOUT 1.10L BY 0.030W. COMPLIEDSDR UPS06548008Bulkhead · chafedNR 2 PYLON AFT BULKHEAD LOWER CORNERS CHAFED ON I/B & O/B SIDES. ACCOMPLISHED REPAIR TO NR 2 PYLON PER FINAL EA 757-27-A1529 AND UPS EO B757-5410-25129-A, WITH NO DEVIATIONS.SDR UPS06548030Frame · dentedINSPECTION TYPE:C DENT IN AFT CARGO FUSELAGE FRAME STA 1540 BET S25L TO S26L (1EA). ACCOMPLISHED REPAIR PER FINAL EA 757-5362-27-A1523 AND UPS EO B757 -5310-25116-A, WITH NO DEVIATIONS.
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