Boeing 757-24APF
Service difficulty reports · 16,054
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 IPXA2025031827619Angle · corrodedAPU INLET DOOR LOWER FWD CORNER ANGLE S-6R HAS CORROSION.REMOVED LOWER FWD ANGLE IAW B757-200PF SRM 51-40-02-0G-0.REMOVE AND REPLACE 1 EACH S-6R CORNER SUPPORT ANGLE (P/N: 148N3141-5) PER PRODUCTION DRAWING REQUIREMENTS AND 757-200PF SRM CHAPTER 51 REQUIREMENTSDR IPXA2025031726547Skin · gougedMAJOR REPAIR, ACCESS DOOR 119BL REAR CUT OUT FUSELAGE, OUTER SKIN HAS (2EA) GOUGES. DOT 72-024 ACCOMPLISHED PER UPS EO: EO-93125-REQI AND VT MAE EA 757-5330-27-A3841SDR IPXA2025030327533Strap · corrodedAPU INLET DOOR STA 1825.00 AFT STRAP HAS CORROSION.REMOVED CORROSION IAW B757-200PF SRM 51-10-02-0G-0 AND EVALUATED IAW SRM 53-80-15-1A-1 TABLE 101.REMOVED FASTENERS IN THE REPAIR AREA IAW B757-200 SRM 51-40-02-0G-0.CUT AND REMOVED THE DAMAGED PART OF THE STRASDR IPXA2025030911672Mount · bentEVAS MOUNTING BRACKET DETACHED INSTALLED NEW MOUNT PLATE WRT EO B757-2560-45127-H, INSTALLED ORIGINAL SERVICEABLE EVAS UNIT FROM PFM IAW AMM 25-69-00. THIS ACTION CLEARS MEL 25-60-1, DMP REVERSED. PLACARD REMOVED.SDR IPXA2025031482551Strap · corrodedFAULT:STR ZONE 300 APU INLET DOOR AT STA 1787.45 FWD STRAP HAS CORROSION. REPLACE 1 EACH APU INLET FORWARD STRAP AT STA 1787.45 (P/N: 148N3138-20) PER PRODUCTION DRAWING REQUIREMENTS AND 757-200PF SRM CHAPTER 51 REQUIREMENTS. INSTALLED NUTPLATE ON STRAP AND ISDR IPXA2025022869424Slat System · faultedLE SLAT DISAGREE AT 190 KTS/ 4000€™ WHEN PLACING FLAP LEVER TO 1. FOLLOWED QRH TO SUCCESSFUL LANDING. REMOVED AND REPLACED #10 RGA ON LEFT WING L/E. OPS CHECK NORMAL PER AMM 27-81-18.SDR IPXA2025022646018Slat System · false indication**EMERGENCY DECLARED**APPROACHING FINAL CALLED FOR FLAPS 1AND SET FLAPS1 AND RECEIVED LE SLAT DISAGREE. PERFORMED THE QRH CHECKLIST LEADING EDGE LIGHT STAYED ILLUM SO WE PERFORMED THE LE EDGE SLAT ASYMMETRY TO ITS T/S PER FIM 27-81 TREE 803 PERFORMED OPERATIONSDR IPXA2025030526691Light · inoperative*SUPPLEMENTAL SDR* INTERIOR EMERGENCY LIGHT INOP ACCOMPLISHED OPS CK OF INTERIOR EMERGENCY LIGHTS IAW AMM 33-51-00. OPS CK GOOD. THIS CLEARS ITEM. PLACARD REMOVEDSDR IPXA2025022426691Light · inoperative**SDR FILED OPEN**INTERIOR EMERGENCY LIGHT INOP DEFERRED PER MEL 33-51-1-1. NO DMP, PLACARED INSTALLED.SDR IPXA2025022783755Retainer · corrodedFAULT: Z193 LH MLG WW DOOR TANG FWD BULB SEAL RETAINER IS EXFOLIATED. VERIFIED REMOVAL OF CORROSION FROM WW DOOR TANG BULB SEAL RETAINER PN 1496016-41. ORIGINAL THICKNESS .050,.046 MATERIAL REMAINING FINDING THE RETAINER TO BE WITHIN LIMITS IAW SRM 53--00-71-1SDR IPXA2025022640252Stringer · punctured**SDR FILED OPEN** AIRCRAFT FUSELAGE PUNCTURED APPROXIMATELY 9FT AFT OF LOWER AFT CARGO DOOR MATERIAL IDENTIFICATION: DOUBLER P/N 2024T3 .063", PO# SP2772414, SNR LOT# 5696144. FILLER P/N 2024T39 .056", PO# SP1818420, SNR LOT# 5995. STRINGER SPLICE P/N BAC149SDR IPXA2025022044028Lever · bindingCAPTAINS WINDOW UNLOCK LEVER HARD TO MOVE. ACCOMPLISHED ADJUSTMENT OF N2 WINDOW IAW AMM 56-11-02-825-001 REV 136. OPERATIONAL TEST IAW AMM 56-11-02-715-020 REV 136 SATIS.SDR IPXA2025022507366Lamp · inoperative**SUPPLEMENTAL SDR**EMERGENCY EXIT LIGHT DIM RELAMPED EMERGENCY EXIT SIGN PER AMM TASK 33-51-01-962-001. OPS COS NORMAL. THIS CLEARS AUTH:2837083. PLACARD REMOVED.SDR IPXA2025022013683Proximity Switch · out of adjustON APPROACH AT APPROX 2000€™ WE RECEIVED A L FWD ENT DOOR EICAS AS WELL AS AN OVERHEAD DISCREET ENTRY DOORS LIGHT. EXTINGUISHED AFTER LANDING. FOUND PROXIMITY SWITCH OUT OF PROPER ADJUSTMENT. ADJUSTED PER AMM 52-71-00. OPS CHECK NORMAL. REMOVED ICE AND SNOW CSDR IPXA2025021907366Light · malfunctionedEMERGENCY EXIT LIGHT DIM 11 LIGHT BULBS INOP. ORDERED PARTS, DEFERRED IAW MEL 33-51-1-1. PLACARD INSTALLED OPENSDR IPXA2025021913683Proximity Switch · out of adjustON APPROACH AT APPROX 2000€™ WE RECEIVED A L FWD ENT DOOR EICAS AS WELL AS AN OVERHEAD DISCREET ENTRY DOORS LIGHT. EXTINGUISHED AFTER LANDING. FOUND PROXIMITY SWITCH OUT OF PROPER ADJUSTMENT. ADJUSTED PER AMM 52-71-00. OPS CHECK NORMAL. REMOVED ICE AND SNOW CSDR IPXA2025021905505Fseu · faulted**ATB** AFTER TAKEOFF MASTER WARNING GEAR NOT DOWN FOLLOWED BY GEAR DOOR. JACKED AIRCRAFT. RETRACTED LANDING GEAR.IMMEDIATELY HAD GEAR NOT DOWN WARNING. FOUND WARNING WOULD CEASE WITH #1 FSEU REMOVED FROM RACK.. REPLACE #1 FSEU PER MM 27-51-01-422-011. NO WARNSDR IPXA2025021805505Landing Gear · malfunctioned**ATB** AFTER TAKEOFF MASTER WARNING GEAR NOT DOWN FOLLOWED BY GEAR DOOR. PER CREW DEBRIEF. AT APPROXIMATELY 1000 FEET AGL FLAPS AT 5, GEAR HANDLE WAS MOVED TO UP. NO GEAR NOISE WAS HEARD, NO INDICATION OF UNLOCK. LANDING CONFIG WARNING CAME ON. GEAR HANDLE SDR IPXA2025030354337Fastener · missingFAULT-STR-ZONE 400. ENG #2 O/B T/R FWD UPPER CHANNEL HAS (1EA) FASTENER MISSING. DOT 28-81. INSTALLED FASTENER (1EA) AT ENG #2 O/B T/R FWD UPPER CHANNEL, IAW B757-200PF 51-40-02. FASTENER P/N CR3212-5-04, BATCH#: 0004334085. REVIEWEDSDR IPXA2025030636262Access Door · delaminatedPANEL 532HZ IS DELAMINATED.ACCOMPLISHED REPAIR PER 757-200PF SRM REV 122 CHAPTER 51-70-07 (250 DEGREE CURE), PER SRM 57-20-09-2R-1.CLEANED & EVALUATED PANEL 532HZ AND FOUND IT TO BE REPAIRABLE IAW 757-SRM-51-70-07-0G-0 PARA 5.J & PARA 5.H FIG.13.PREPARED AND ASDR IPXA2025030636145Panel · delaminatedCOMP DRY BAY DOOR CUT OUT HAS COMPOSITE DELAM. ACCOMPLISHED REPAIR PER VT-MAE EA 757-5720-27-A3804.SDR IPXA2025021422413Landing Gear · warning messageDURING CLIMB OUT (AFTER TAKEOFF) MASTER WARNING GEAR NOT DOWN FOLLOWED WITH WARNING GEAR DOOR. AFTER REPLACEMENT OF S488 AND M983, VERIFIED GEAR NOT DOWN MESSAGE IS NOT PRESENT WITH GEAR UP AND THROTTLES ADVANCED. VERIFIED MESSAGE PRESENT WITH THROTTLES AT SDR IPXA2025021322413Circuit Card · malfunctionedDIVERSION, DURING CLIMB OUT (AFTER TAKEOFF) MASTER WARNING GEAR NOT DOWN FOLLOWED WITH WARNING GEAR DOOR PER REQUEST OF TECH SUPPORT CHECKED PSEU. NO DEFECTS FOUND. TECH NOW SUSPECTS BAD LANDING GEAR CONFIGURATION CARD IN PSEU. OPENSDR IPXA2025021397102Strip · crackedFAULT-STR- ZONE 420, ACCESS PANEL 425BL METAL STRIP EDGE CRACKED. DOT 68-16.REMOVED SEAL, HINGE-REAR WITH CRACK IAW SRM B757-200 TASK: 51-40-02.INSTALLED NEW SEAL, HINGE-REAR WITH (3EA) NAS1097AD4-7 BATCH: 0003968643 IAW SRM B757-200 TASK: 51-40-02.SDR IPXA2025022693724Floor Panel · crackedFAULT-STR-ZONE 100. AFT CARGO COMPT FLOOR PANEL 153BF HAS A CRACK. DOT 28-57.FABRICATED NEW FLOOR PANEL 153BF IAW GMM 09.08.01.03.SDR IPXA2025021378219Bracket · crackedFAULT: STR Z800 FWD LWR CARGO DOOR HAS A CRACK IN AN "L" BRACKET LOCATED IN THE FWD UPPER CORNER. DOT 06677-03.INSTALLED BRACKET WITH (3EA) BACR15FT6D6C, BATCH: 0004364973 & (2EA) CR3213-6-05, BATCH: 0004214429 & (1EA) HL12VF6-6, BATCH: 0004208818 & (1EA) MS2SDR IPXA2025021271069Skin · crackedLH WING LEADING EDGE UPPER SURFACE AT SLAT #4 LOCATION, HAS 1 CRACK. DOT 28-38. MADE A REPLACEMENT SKIN FROM 2024-T3 CLAD SHEET, 0.100''. PER E.A. #: 757-5741-27-A3790 PRELIMINARY 1, STEP 8. P/N: 2024-T3 .100C, BATCH: 0004322815. INSTALLED FASTENERS CODE A, B SDR IPXA2025030374205Angle · corrodedFAULT: STR Z-300 APU INLET DOOR FWD LOWER CORNER ANGLE 148N3141-5 IS CORRODED. INSTALLED LOWER CORNER ANGLE PER SRM 51-40-02. REVIEWEDSDR IPXA2025021774058Strap · corrodedFAULT: STR Z-300 APU INLET DOOR FWD STRAP 148N3138-20 IS CORRODED. INSTALLED FWD STRAP IAW SRM 51-40-02 RIVET P/N BACR15CE8KE7 BACH#4256147. REVIEWEDSDR IPXA2025021577164Floorbeam · corrodedFAULT-STR- ZONE 142 MAIN CARGO COMPARTMENT RIGHT SIDE STA 1020, BL 0 TO RBL 24.5 FLOOR BEAM SUPPORT CHANNEL SPOTS WITH CORROSION. CLEANED MAIN CARGO COMPARTMENT /RH SIDE STA 1020, BL 0 TO RBL 24.5 FLOOR BEAM SUPPORT CHANNEL IAW SOPM 20-30-03. AFTER FURTHER INSDR IPXA2025021577074Support Channel · corrodedMAIN CARGO COMPARTMENT LEFT SIDE STA 1050 BL 0 TO LBL 24.5 FLOOR BEAM SUPPORT CHANNEL SPOTS WITH CORROSION. DOT 68-02 FR-68. LOCATED AND DRILLED NEW TEE SUPORT IAW SRM B757-200 TASK: 51-40-05. INSTALLED NEW TEE IAW SRM B757-200 TASK: 51-40-02.SDR IPXA2025022576954Floorbeam · corrodedMAIN CARGO COMPARTMENT LEFT SIDE STA 1050 LBL 45.5 TO LBL 65.5 FLOOR BEAM SUPPORT CHANNEL SPOTS WITH CORROSION. DOT 68-01 FR-68. REMOVE AND REPLACE 1 EACH FLOORBOARD SUPPORT TEE (P/N: 144N5005-4) PER PRODUCTION DRAWING REQUIREMENTS AND 757-200PF SRM CHAPTER 51SDR IPXA2025021674009Angle · corrodedAPU INLET DOOR UPPER ANGLE 148N3152-2 IS CORRODED. INSTALLED UPPER ANGLE IAW SRM 51-40-02.SDR IPXA2025072360023Skin · damagedMAJOR REPAIR. IMPACT DAMAGE TO FUSELAGE SKIN BS 1340, S25. REPAIRED IAW EO-91018-REQ3.SDR IPXA2025020960023Skin · ground damageMAJOR REPAIR, IMPACT DAMAGE TO FUSE. SKIN STA. 1340 STR. 25L (REFERENCE SRM 53-60-01-0I-1, FIGURE 1, DETAIL II, ITEM 2). THE DAMAGE CONSISTS OF A DENT TO THE FUSELAGE SKIN PANEL. THE DENT MEASURES APPROXIMATELY 10.5IN CIRCUMFERENTIALLY BY 2.0IN FWD/AFT WITH ASDR IPXA2025021955007Skin · nickedUPPER FUS. EXTERNAL SKIN AROUND LH GPS ANTENNA STA 670 STR 1L-2L WITH NICKS (5 SPOTS)-DOT 139/14-MR/139.RESTORED SURFACE PROTECTION ON EXTERNAL SKIN AROUND LH GPS ANTENA STA 670 STR 1L-2L IAW SRM 51-20-01 AND AMM51-21-15.SDR IPXA2025021760646Cam · gougedMAIN CREW DOOR LWR CAMLATCH HAS GOUGE ON OUTER SURFACE. DOT 69/006. EL-69. BLEND OUT GOUGE ON MAIN CREW DOOR LWR CAMLATCH IAW B757-200PF, SRM 51-10-02. SURFACE HFEC PERFORMED ON MAIN CREW DOOR LOWER CAM LATCH BLENDED AREA. NO DEFECTS FOUND IAW NTM 51-00-21 TSDR IPXA2025021760600Latch · gougedMAIN CREW DOOR UPPER CAMLATCH HAS GOUGE ON OUTER SURFACE. DOT 69/005. EL-69. SURFACE HFEC PERFORMED ON MAIN CREW DOOR UPPER CAM LATCH BLENDED AREA. NO DEFECTS FOUND IAW NTM 51-00-21 T96525.SDR IPXA2025021060646Cam · gougedMAIN CREW DOOR LWR CAMLATCH HAS GOUGE ON OUTER SURFACE.SDR IPXA2025021060600Cam · gougedMAIN CREW DOOR UPPER CAMLATCH HAS GOUGE ON OUTER SURFACE.SDR IPXA2025020848485Floorbeam · corrodedFAULT: Z100 STR FS 1240 RBL 22 TO RBL 30 FWD FLANGE OF LOWER TEE CHORD HAS SEVERE INTERGRANULAR CORROSION. INSTALLED T-CHORD AN ANGLES ON STR FS 1240 RBL IAW B757-200 SRM 51-40-02 AND SRM 51-70-12-0G-0 DETAIL VIII FIGURE 1 SHEET 7. REVIEWEDSDR IPXA2025022851520Floorbeam · corrodedFAULT: Z100 STR FS 900 BETWEEN RBL 12 TO RBL 16.5 LOWER TEE CHORD HAS CORROSION. INSTALLED OUTBOARD CHORD AND 8(EA) REPAIR PLATES AT STA 900 I.A.W SRM 51-70-12-OG AND SRM 51-40-02-OG. REVIEWED.SDR IPXA2025022751440Floorbeam · corrodedFS 1037 RBL 59 LOWER TEE CHORD HAS CORROSION FWD AND AFT FLANGE. RESTORED SURFACE PROTECTION AT NEW T-CHORD IAW B757-200PF SRM 51-20-01-0G-0. ALODINE P/N; ALODINE1132 B/N;0004315010 PRIMER P/N;10-P4-2/2TU B/N; 0004341746 PAINT WHITE P/N; PG6-W2K4Q B/N; 4361130SDR IPXA2025020848535Tee Angle · corrodedFS 1238- FS 1240 RBL 31 INBD LOWER TEE CHORD FLANGE HAS SEVERE INTERGRANULAR CORROSION. REMOVE AND REPLACE 1 EACH RBL 30.75 (P/N: 149N7633-14) LOWER TEE CHORD AT STA 1240 PER PRODUCTION DRAWING REQUIREMENTS AND 757-200PF SRM CHAPTER 51 REQUIREMENTS. VERIFIED ISDR IPXA2025020933681Strap · corrodedAPU INLET DOOR AT STA 1825 AFT STRAP HAS CORROSION.ACCOMPLISHED REPAIR PER 757-200PF SRM REV 122 CHAPTER 53-80-15-2R-1, DETAIL I ON FIGURE 202 (SHEET 2).SDR IPXA2025021200052Window · overheatedL/H #1 WINDOW SHOWING SIGNS OF WINDOW HEAT OVERHEAT/ARCING DAMAGE INSTALLED L1 WINDOW IAW AMM 56-11-01 UP TO AERO DYNAMIC SEALANT REF T3F18E0061ZX1REF T3F18E0061ZX1 FOR AERO DYNAMIC SEALANT DEFERRALSDR IPXA2025021215360Fuel Sys · out of balanceIN FLIGHT FUEL IMBALANCE OF 2KLBS DEVELOPED WITH RIGHT SIDE LESS. WE BALANCED IT. 1HR LATER DURING ARRIVAL RIGHT SIDE WAS 1KLBS LESS THEN THE LEFT AGAIN ON SHORT FINAL FMC TOTALIZER FUEL SHOWED 9.9L WORK PERFORMED UNDER TASK CARD #T3F18E005Z998: R/R CTR TK, FWSDR IPXA2025020715360Fuel Sys · out of balanceIN FLIGHT FUEL IMBALANCE OF 2KLBS DEVELOPED WITH RIGHT SIDE LESS. WE BALANCED IT. 1HR LATER DURING ARRIVAL RIGHT SIDE WAS 1KLBS LESS THEN THE LEFT AGAIN ON SHORT FINAL FMC TOTALIZER FUEL SHOWED 9.9. OPENSDR IPXA2025020600052Window · overtempL/H #1 WINDOW SHOWING SIGNS OF WINDOW HEAT OVERHEAT/ARCING DAMAGE.SDR IPXA2025020601773Pump · inoperativeCENTER TANK FUEL PUMPS DO NOT SHUT OFF WHEN SELECTED OFF. R/R LFT CTR OVERRIDE BOOST PUMP PER AMM 28-22-03. OPS CHECK NORMAL, NO LEAKS NOTICED.
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