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 IPXA2026023834460Seat Track · dentedMAIN CARGO COMPARTMENT FLOOR STRUCTURE, BL 0 SEAT TRACK HAS (1EA) DENT. REMOVED DAMAGED SECTION OF SEAT TRACK IAW SRM 53-00-52-2R-7 STEP 2 AND SRM 51-40-02-0G-0 INSTALLED REPAIR PARTS IAW SRM 53-00-52-2R-7, STEP 10, AND SRM 51-40-02-0G-0.SDR IPXA2026021939888Support Angle · corrodedMAIN CABIN FLOOR STRUCTURE, STA 1720 LBL 20 LOWER NUTPLATE ANGLE SUPPORT CORRODED. REMOVED LOWER NUTPLATE ANGLE SUPPORT CORRODED I.A.W. B757-200 SRM 51-40-02-0G-0 INSTALLED LOWER NUTPLATE ANGLE SUPPORT I.A.W. 757-200 SRM 51-40-02-0G-0..SDR IPXA2026021939793Support Angle · corrodedMAIN CABIN FLOOR STRUCTURE, STA 1720 LBL 45 LOWER NUTPLATE ANGLE SUPPORT CORRODED. DOT 28-05 .REMOVED LOWER NUTPLATE ANGLE SUPPORT CORRODED I.A.W. B757-200 SRM 51-40-02-0G-0 INSTALLED LOWER NUTPLATE ANGLE SUPPORT I.A.W. 757-200 SRM 51-40-02-0G-0.SDR IPXA2026021940348Support Angle · corrodedMAIN CABIN FLOOR STRUCTURE, STA 1720 RBL 10 LOWER NUTPLATE ANGLE SUPPORT CORRODED. REMOVED LOWER NUTPLATE ANGLE SUPPORT CORRODED IAW SRM 51-40-02-0G-0 INSTALLED LOWER NUTPLATE ANGLE SUPPORT IAW SRM 51-40-02-0G-0.SDR IPXA2026021241625Deck Plate · corrodedMAIN CABIN FLOOR STRUCTURE, DECK PLATE STA 1700-1720 BL0 -RBL 50 HAS 15EA AREAS WITH CORROSION. REMOVED CORROSION IN 15 AREAS. MAIN CABIN FLOOR STRUCTURE, DECK PLATE BS 1700-1720, BL0 -RBL 50.IAW SRM 51-10-02 TABLE 101. RESTORED SURFACE PROTECTION IAW.SRM 5SDR IPXA2026022092281Seat Track · corrodedSTR--UPON VERIFICATION OF REMOVAD FROZEN BOLT AT FWD SIDE OF SEAT TRACK SECTION IN MAIN CABIN STA 880 LBL 20 FOUND CORROSION--ATA 53 MARKED 007-02 REMOVED DAMAGE SECTION OF WEB (SIDE PANEL). IAW WITH SREO-3220-REQ003 AND SRM 51-70-13 STEP 1. INSTALLED REPAISDR IPXA2026021874039Bracket · corrodedACCESS DOOR 313AL LH AND RH LATCH STOPS AT THE CUT-OUT, 4EA BRACKETS ARE CORRODED. REMOVED 4EA BRACKETS WITH CORROSION I.A.W. SRM 51-40-02-0G-0. INSTALLED 4EA BRACKETS ACCESS DOOR 313AL LH AND RH LATCH STOPS AT THE CUT-OUT IAW B757-200 SRM 51-40-02.SDR IPXA2026021188165Skin · crackedAFT CARGO DOOR EXTERNAL SKIN HAS A 2" CRACK APPROX. AT THE LOWER AFT SECTION. DOT 21-01 THIS REQUIRES SUPPLIMENTAL INSPECTION AT THRESHOLD OF 37,500 FC REPEAT INSPECTION WITHIN 3000 FC DEFERRED IAW B757-200PF SRM 52-30-2R-4, REPAIR 4.SDR IPXA2026022369212Skin · crackedLT WING FIXED L/E UPPER COMPOSITE SKIN HAS CRACKS UNDER SLAT NR 4. EVALUATED LT WING FIXED L/E UPPER COMPOSITE SKIN UNDER SLAT NR 4. FOUND OUT OF LIMITS, IAW SRM 57-41-01-1A-1, TABLE 1 FIGURE 101 ACCOMPLISHED REPAIR PER EO-96538-REQ1 AND VT-MAE EA 757-5741-SDR IPXA2026020247576Handle · brokenCREW ENTRY WAY ASSIST HANDLE BROKEN. REPLACED THE CREW ENTRYWAY ASSIST HANDLE IAW IPC 52-12-51-01.SDR IPXA2026020246985Lamp · inoperativeEMERGENCY EXIT LIGHT- MANY LAMPS INOP. RELAMPED ALL EMERGENCY EXIT LIGHT, OPS CHECKS NORMAL IAW AMM 33-51-00-501.SDR IPXA2026013038362Charger · no testEMERGENCY EXIT LIGHT WILL NOT TEST REMOVED AND REPLACED EMERGANCY LIGHT BATTERY ASSY AND BATTERY CHARGER REF 757MM 33-51-07-902-001 33-51-07-862-054 TEST OK. OK FOR SERVICESDR IPXA2026012925317Window · crackedLT FWD WINDOW CRACKED. REMOVED AND REPLACED L1 WINDOW IAW B757 AMM 56-11-01 OPS AND LK CHECKS GOOD AT THIS TIME. PERFORMED RII OF L1 WINDSHIELD ELECTRICAL CONNECTION INSTALL AND TORQUE PER GMM 04-02.SDR IPXA2026012925306Element · burnedLEFT FWD WINDOW LOWER ELEMENT BURN OUT DURING FLIGHT. REPLACEED THE L1 WINDSHIELD. ALSO REPLACED M191 HEAT CONTROL UNIT PRECAUTIONARY PER AMM 30-41-01-004-001. OPS CHECK GOOD. REF BARCODE T3F18E0086B65 FOR RII SIGNOFF OF L1 WINDSHIELD REPLACEMENT.SDR IPXA2026021699522Seat Track · damagedWHEN TRYING TO REMOVE THE UPPER BUSHING OF THE BROKEN LINK P/N 143N5096-2 WHICH FOUND SEIZED ON ASSY. 143N5405-920, TRACK ASSY AFT HOLE FOUND ELONGATED. SEE ATTACHED PICS. REMOVED ASSY 143N5405-920 WITH HOLE ELONGATED I.A.W. B757-200 SRM 51-40-02-0G-0 INSTALLSDR IPXA2026021096944Stiffener · cracked# 2 PYLON ANGLE IS CRACKED INSIDE PANEL 445AL , ATA 54 STR. INSTALLED (1EA) NEW SPAR STIFFENER, (1EA) WEB CHANNEL (INBD) AND (1EA) WEB CHANNEL (OUTB) PREVIOUSLY REMOVED FOR ACCESS AT #2 PYLON INNER SIDE ABOVE EXHAUST IAW B757-200PF SRM 51-40-02-0G-0 PER E.A.#:SDR IPXA2026012891803Controller · faultedEMERGENCY DECLARED, CABIN ALTITUDE WARNING EICAS ABOVE 100 MSL. A/C @ FL 210/CABIN ALT 11500/ WARNINGS OCCURRED WITH BOTH PACKS RUNNING. REMOVED AND REPLACED #2 AUTO CABIN CONTROL UNIT IAW AMM 21-31-02. OPS CHECK GOOD, PLACARD REMOVED.SDR IPXA2026012791803Warning Message · illuminatedEMERGENCY DECLARED, CABIN ALTITUDE WARNING EICAS ABOVE 100 MSL. ACFT AT FL 210, CABIN ALT 11500. WARNINGS OCCURRED WITH BOTH PACKS RUNNING. THIS ITEM WAS DEFERRED IAW MEL 21-31-1A, VERIFIED MANUAL OPERATION OF OUTFLOW VALVE.SDR IPXA2026072066283Floor Panel · damagedMAJOR REPAIR, MCD FLOOR PANEL 242XEF DAMAGED INSTALLED FLOOR PANEL 242XEF REF AMM 53-01-01SDR IPXA2026012666283Floor Panel · damagedMAJOR REPAIR. MCD FLOOR PANEL 242XEF DAMAGED REF ATTACHED IMAGES. CRACK IS ON AFT SIDE TOP FACE OF PANEL. APPROX 15.5€? IN LENGTH. 1€?-1.5€? FROM AFT SIDE OF PANEL. 1.5€? FROM LEFT AND RIGHT SIDES OF PANELSDR IPXA2026012743275Floor Support · corrodedFLOOR SUPPORT ANGLE AT APPROX STA 1715 OUTBOARD L/H SIDE, IS CORRODED JUST FWD OF AFT PRESSURE BULKHEAD. DOT AA023. STR ATA 51-00 REMOVED DAMAGED FLOOR SUPPORT ANGLE FROM APPROX STA 1715 OUTBOARD L/H SIDE JUST FWD OF AFT PRESSURE BULKHEAD REF. B757-200PF SRM 5SDR IPXA2026012343275Floor Support · corrodedAGING ACFT INSP - FLOOR SUPPORT ANGLE AT APPROX STA 1715 OUTBOARD L/H SIDE, IS CORRODED JUST FWD OF AFT PRESSURE BULKHEAD. DOT AA023. STR ATA 51-00SDR IPXA2026020125876Seat Track · corrodedCORROSION ON SEAT TRACK IN CABIN AT STA 1066 LBL 47", 4-003 ATA 53 STR AUDITED<BR>CPCP AND SDR SUBMITTEDSDR IPXA2026022401372Angle · corrodedSTR, ATA 55: R/H HORZ STAB TO ELEVATOR MOST OTBD HINGE BONDING STRAPS ATTACH BRACKETS BLOW OUT WITH CORROSION AND BOTH BONDING STRAPS (2 EACH) FRAYED AND CORRODED. RL013 INSTALLED BONDING STRAP P/N BACJ40E20-20 BATCH 0004458634, BONDING BRACKET (ANGLE) AND WEBSDR IPXA2026022402462Angle · corrodedLEFT HORZ STAB TO ELEVATOR MOST OTBD HINGE BONDING STRAPS ATTACH BRACKETS HAVE CORROSION AND BOTH BONDING STRAPS (2 EACH) FRAYED AND CORRODED. RL029 INSTALLED 1EA ANGLE, 1EA WEB AND 1EA BONDING STRAP AT LH HORIZONTAL STABILIZER STAB STA 360 IAW 757-200PF SRM 5SDR IPXA2026020184023Bracket · corrodedRH HORZ STAB REAR SPAR BEHIND HORZ TIP FAIRING, BONDING WIRE ATTACHED BRACKET IS CORRODED (059-07) INSTALLED BONDING WIRE ATTACHED BRACKET P/N 183N1341-2 ON RH HORZ STAB REAR SPAR BEHIND HORZ TIP FAIRING IAW B757 SRM 51-40-02-OG-O. REVIEWEDSDR IPXA2026021193646Angle · corrodedSTR- BROKEN NUT PLATE ON RH AFT WING TO BODY JUST ABOVE RAM AIR TURBINE MARKED JK200-25 ATA 53-40. INSTALLED 01 EA TEE CHORD LOWER BEAM P/N 149N7630-38 BATCH 0004458867 (STA 1180-STA 1240) AND (1EA) INTERCOSTAL PREVIOUSLY REMOVED FOR ACCESS AT STA 1240 THRU 1SDR IPXA2026012386466Flap System · faultedAIR TURN BACK, TE FLAP ASSYMETRY. PERFORMED OPS CHECK OF FLAP SYSTEM IAW AMM 27-51-00-715-001. OPS CHECK NORMAL. ALSO VERIFIED FLAP POSITION TRANSMITTERS IAW AMM 27-58-01-825-003 STEPS 2.I. AND 2.J. ALL VALUES WITHIN LIMITS.SDR IPXA2026012086466Flap System · faultedAIR TURN BACK, TE FLAP ASSYMETRYSDR IPXA2026022323794Strap · corrodedCORROSION FOUND ON APU INLET SURROUND STRUCTURE FWD STRAP O/B END . ATA 53 ,STR INSTALLED 4EA STRAP ANGLES AT APU INLET SURROUND STRUCTURE FWD IAW B757-200PF-SRM 51-40-02-0G-0SDR IPXA2026011613640Unknown · odorAT APPLICATION OF TAKEOFF POWER AND DURING CLIMB-OUT, THE STRONG ODOR OF DIRTY WET SOCK EXISTED. THE SMELL LESSENED A BIT DURING CRUISE BUT WAS STILL NOTABLY PRESENT FOR THE REMAINDER OF THE FLIGHT. PERFORMED FIM. INSPECTED POSSIBLE SOURCE AREAS, NO SOURCE NSDR IPXA2026011513640Unknown · odorAT APPLICATION OF TAKEOFF POWER AND DURING CLIMB-OUT, THE STRONG ODOR OF DIRTY WET SOCK EXISTED. THE SMELL LESSENED A BIT DURING CRUISE BUT WAS STILL NOTABLY PRESENT FOR THE REMAINDER OF THE FLIGHT. AT SDF MGMT REQUEST, OPERATED LEFT AND RIGHT AIR PACKS FOR APSDR IPXA2026012304472Web · damagedSTA 1200 UPPER WEB HAS A DAMAGED HOLE. AFTER FURTHER EVALUATION FOUND 4 DOUBLE HOLE AT THE TOP OF THE WEB. FOUND OUT OF LIMITS IAW B757-200 SRM 53-00-71-1A-1 AD1. CUT AND REMOVE DAMAGED SECTION OF WEB. IAW B757-200 SRM 51-70-13-0G-0 STEP 1. ++INSTALLED REPAIRSSDR IPXA2026011477249Flap System · faultedFLAP/SLAT ELEC STATUS MESSAGE TRAILING EDGE FLAPS DISAGREE EICAS RAN CHECK LIST LANDED FLAP 20*. ACCOMPLISHED ADJUSTMENT OF FLAP SYSTEM IAW AMM 27-51-00-825-007.REMOVED AND REPLACED FLAP POSITION INDICATOR IAW AMM 27-58-02-004-001 DUE TO A FAULTY (L) NEEDLE SDR IPXA2026011377249Warning Message · illuminatedEMD, FLAP/SLAT ELEC STATUS MESSAGE TRAILING EDGE FLAPS DISAGREE EICAS RAN CHECK LIST LANDED FLAP 20*SDR IPXA2026011963930Seat Track · corrodedCAP SEAT TRACKS HAVE EVIDENCE OF CORROSION (AFT I/B EXFOLIATED) MARKED AREAS. REMOVED CORROSION LOCATED ON MAIN DECK FLOOR SHEAR UNDER SEAT TRACK. LBL13.0 AND 20'' UPPER STA278.0 O.T: .050''. MAT LOSS:0.035''. L:0.7'', W:0.7'' REWORK WAS FOUND OUT OF LIMITS ISDR IPXA2026020462981Stringer · corrodedFUSELAGE SKIN IS BULDGING AROUND TWO FASTNER HEADS, JUST FORWARD OF THE AFT LOWER FUSELAGE MAJOR REPAIR AT AFT VHF ANTENNA. REMOVED 3 BULDGING RIVETS FORWARD OF THE AFT LOWER FUSELAGE MAJOR DOUBLER REPAIR AT STATION 1460 AND FRAME 1480 OF AFT VHF ANTENNA, NOSDR IPXA2026013069167Tee Angle · corrodedWING TO BODY FAIRING STRUCTURE LOWER T-CHORD EXFOLIATED AND WITH MULTIPLE SPOTS OF HEAVY CORROSION FROM BS 1180 TO 1240 AT RBL 57.50. DOT 21-40. EVALUATED TEE FITTING BETWEEN STA 1180-1240 AT RBL 57.5 AND FOUND TO BE EXFLOIATED WITH 100% MATERIAL LOSS AND ISSDR IPXA2026012869037Tee Fitting · corrodedWING TO BODY FAIRING STRUCTURE UPPER TEE FITTING EXFOLIATED AND WITH MULTIPLE SPOTS OF HEAVY CORROSION FROM BS 1180 TO BS 1240, RBL 57.50. REMOVED AFT WTB PANEL 198LR TO FOM IAW AMM 53-66-01-004-001. INSTALLED THE TEE FITTING IAW SRM 51-40-02.SDR IPXA2026012868936Channel · corrodedWING TO BODY FAIRING SUPPORT STRUCTURE WITH EXFOLIATED CORROSION AT BS 1219 RBL 6. INSTALLED NEW CHANNEL, 2EA SUPPORT PLATES, 1EA ANGLE, IN WING TO BODY, BS 1219 RBL 6, IAW B757 SRM 51-40-02-0G-0.SDR IPXA2026012869140Tee Fitting · corrodedWING TO BODY FAIRING STRUCTURE, VERTICAL T-FITTING EXFOLIATED AT LWR END AT BS 1200 RBL 57.50. INSTALLED T-FITTING IAW SRM 51-40-02.SDR IPXA2026012369147Tee Fitting · corrodedRIGHT WW EXTERNAL STRUCTURE BETWEEN BS 1040 - 1060 INTERCOSTAL DELAMINATED. INSTALLED NEW T-FITTING, IAW SRM 51-40-02-0G-0.SDR IPXA2026012769147Intercostal · delaminatedRIGHT W/W EXTERNAL STRUCTURE BETWEEN STA 1040 TO 1060 INTERCOSTAL WITH DELAMINATION DOT 07-060 REVIEWEDSDR IPXA2026011955833Skin Panel · corrodedAPU BAY, INTERNAL STRUCTURE RT SIDE, BTWN BS 1885.2 & 1918.9, ALUMINUM HONEYCOMB SKIN HAD CORROSION. TRIMMED OUT LOWER FWD SECTION OF HONEYCOMB ONLY ON SKIN BOND ASSY. PANEL TO REMOVE EXFOLIATED CORROSION, ACCOMPLISHED AND INSPECTION OF THE STRINGER AND SURROSDR IPXA2026013056128Longeron · corrodedAPU BAY, INTERNAL STRUCTURE RT LONGERON, BS 1885.2 CORRODED. REMOVED CORROSION ON THE RT APU LONGERON, ORIGINAL THICKNESS 0.050", MATERIAL REMOVED 0.008". INSTALLED NEW LONGERON, SERVICABLE SEAL RETAINER, SERVICABLE SUPPORT PLATES, SERVICABLE HINGE ASSY, SSDR IPXA2026013056154Intercostal · crackedMDC DOOR INTERNAL STRUCTURE, AN INTERCOSTAL FOUND CRACKED AT FWD LWR SECTION. REMOVED THE INTERCOSTAL IAW SRM 51-40-02-0G-0, AFTER EVALUATION FOUND CRACK TO BE OUT OF LIMITS, FLANGE 1.095", LENGTH 0.940", IAW 52-30-02-1A-1, DETAIL II, NOTE B. INSTALLED NEW ISDR IPXA2026012356310Tee Fitting · corrodedLOWER FUSELAGE RT SIDE STA 1200 T-FITTING EXFOLIATED. INSTALLED A NEW T-FITTING IAW SRM 51-40-02-0G.SDR IPXA2026012353616Tee Angle · corrodedEXTERNAL FUSELAGE LT W/W BETWEEN STA 1060 TO 1080 INTERCOSTAL HAS CORROSION. INSTALLED NEW T-CHORD / INTERCOSTAL I.A.W. B757-200 SRM 51-40-02-0G-0.SDR IPXA2026011253273Anti-Ice Valve · faulted**ATB** DURING CLIMB R ENG ANTI ICE DISPLAYED RUN QRH CHECKLIST. CONSULTED WITH FLT CONTROL AND RETURNED TO MIA DUE TO WX IN SDF. REMOVED AND REPLACED RH ENG INLET TAI VALVE AMM 30-21-03. OPS CHECKS NORMAL. NO LEAKSSDR IPXA2026012234008Skin · crackedLEFT WING FIXED LEADING EDGE SKIN UPPER SURFACE HAS A GOUGE, AREA BY SLAT NR 1 OTBD END. PERFORMED CUT OUT OF THE AFFECTED PANEL FROM THE CENTER LINE OF THE MAIN TRACK AT OSS 809.46 TO THE OTBD END OF PANEL, IAW EA 757-5741-27-A4274 PRELIMINARY 1, STEP 3. IN
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