Boeing 757-23A
Service difficulty reports · 1,397
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 = '75723A' 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 = '75723A' 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 FDEA201912133242Floor Panel · damagedAFT CARGO PANEL # 161AF DAMAGED REPLACED AFT CARGO PANEL 161AF IAW FEDEX GMM 7-0-1001 AND BOEING DRAWING # 453N1805.SDR FDEA201912133240Structure · corrodedL/H ELEVATOR TIP CORRODED. REMOVED L/H ELEVATOR TIP CORROSION AND FOUND TO BE OUTSIDE LIMITS IAW SRM 55-20- 01-1A. ELEVATOR TIP REPAIRED IAW FEDEX EA # F-5520-T0351151.SDR FDEA201912133239Strip · corrodedEVIDENCE OF LIGHT SURFACE CORROSION AT L/H ELEVATOR UPPER AND LOWER CONDUCTIVE STRIPS, LOCATED AT OUTBOARD END , (ELEV. STA 312 APPROX) REMOVED CORRODED SPLICE PLATES UPPER AND LOWER AND FOUND TO BE CORRODED BEYOND LIMITS IAW SRM 55-20-01-1A. UPPER ANDSDR FDEA201912103217Skin · debondedSLAT #7 HAS DISBOND ON T/E WEDGE UPPER SURFACE REPLACED SLAT #7 IAW AMM 27-81-02 IAW AMM 27-81-02SDR FDEA201912103216Skin · puncturedPUNCTURE FOUND ON LH ELEVATOR UNDER O/B STATIC DISCHARGER BASE AFTER REMOVAL OF DISCHARGER BASE PUNCTURE ON LH ELEVATOR UNDER O/B STATIC DISCHARGER BASE REPAIRED IAW SRM 51-70-17-0G, EA F-5520-T0351138 P1 .SDR FDEA2023012713215Skin · dentedDENT ON L/H WING I/B MAIN FLAP 6" FROM T/E, 9" O/B OF AFT FLAP UPPER PUSH ROD FITTING, LOWER SURFACE. REPAIRED PUNCTURE TO FLAP IAW SRM 51-70-10-2R REPAIR 4 AND SRM 51-70-03-0G AND FEDEX EA #F-5750-T0351164SDR FDEA2019121303214Proximity Sensor · inoperativeRIGHT DOOR SLIDE LIGHT DOES NOT ILLUMINATE WHEN ARMED. VERIFIED 28VAC AT SLIDE LIGHT L404. VERIFIED GOOD CONTINUITY THROUGH AFT GIRT BAR PROX SENSOR S10217 WITH THE SWITCH ACTUATED. VERIFIED GOOD GROUND AT GD2922-AC. NO CONTINUITY FOUND THROUGH FWD PROX SESDR FDEA2019121303217Skin · debondedSLAT #7 HAS DISBOND ON T/E WEDGE UPPER SURFACE REPLACED SLAT #7 IAW AMM 27-81-02 IAW AMM 27-81-02SDR FDEA2019121303216Skin · damagedPUNCTURE FOUND ON LH ELEVATOR UNDER O/B STATIC DISCHARGER BASE AFTER REMOVAL OF DISCHARGER BASE PUNCTURE ON LH ELEVATOR UNDER O/B STATIC DISCHARGER BASE REPAIRED IAW SRM 51-70-17-0G FEDEX E.A F-5520-T0351138 P1 STABILISERS- ELEVATORS UPPER SKIN PUNCTURE REPSDR FDEA2019121303215Skin · dentedDENT ON L/H WING I/B MAIN FLAP 6" FROM T/E, 9" O/B OF AFT FLAP UPPER PUSH ROD FITTING, LOWER SURFACE. REPAIRED PUNCTURE TO FLAP IAW SRM 51-70-10-2R REPAIR 4 AND SRM 51-70-03-0G AND FEDEX EA #F-5750-T0351164SDR FDEA2019120973208Bulb · inoperativeSVC CK R-1 DOOR EMERGENCY ESCAPE SLIDE LIGHT INOP. RELAMPED R ESCAPE SLIDE LIGHT REF AMM 33-51-06-2-1, BULB GE767. OP'S NORMAL OK FOR SERVICESDR FDEA2019120653187Beam · corrodedTRANSVERSE BEAM B/S 900 RBL 45 IS CORRODED BEYOND PERMITTED LIMITS IAW SRM 53-00-51-1A, ALLOWABLE DAMAGE 1, DETAIL III REPLACED TRANSVERSE BEAM IAW SRM 51-40-02 AND BOEING DRAWING #111N5201SDR FDEA2019120653186Floorboard · damagedFLOOR PANEL 241MCF BETWEEN BSTA 900 - 1180 L/H WAS FOUND TO BE DAMAGED REPAIRED FLOOR PANEL 241MCF IAW SRM 53-00-50 REV 128 FIBREGLASS BMS 9-3 TY.H B/N:21263471 RESIN BMS 8-201 TY.4 B/N:27782742SDR FDEA201912043170Beam · corrodedTRANSVERSE BEAM B/S 900 - 1040, LBL 46 IS CORRODED BEYOND PERMITTED LIMITS IAW SRM 53-00-51-1A ALLOWABLE DAMAGE 1, DETAIL III. INSTALLED NEW TRANSVERSE BEAM IAW SRM 51-40-02 AND BOEING DRAWING #111N5201SDR FDEA201912033164Beam · corrodedTRANSVERSE BEAM B/S 900-1040 LBL 25 IS CORRODED BEYOND LIMITS IAW SRM 53-00-51-1A ALLOWABLE DAMAGE DETAIL III. REPLACED TRANSVERSE BEAM B/S 900-1040 LBL 25 IAW SRM 51-40-10 AND BOEING DRAWING# 111N5202SDR FDEA2019120433164Beam · corrodedTRANSVERSE BEAM B/S 900-1040 LBL 25 IS CORRODED BEYOND LIMITS IAW SRM 53-00-51-1A ALLOWABLE DAMAGE DETAIL III. REPLACED TRANSVERSE BEAM B/S 900-1040 LBL 25 IAW SRM 51-40-10 AND BOEING DRAWING# 111N5202SDR FDEA2019120423161Beam · corrodedTRANVERSE BEAM B/S 900-1040 RBL 25 CORRODED REPLACED TRANSVERSE BEAM B/S 900-1040 IAW SRM 51-40-02 AND BOEING DRAWING#111N5202SDR FDEA201911263110Light · inoperativePDIS 994 25-60 7876 26NOV19 BUF OPEN U LOGPAGES:3167525 R1 DOOR SLIDE LIGHT NOT ILLUMINATED WHILE ARMED. MEL 26NOV19 00:00 BUF U RELEASED FOR SERVICE PER MEL : 25-66-05-A CATEGORY : C EXPIRATION : 06DEC19 "MEL 25-66-05-A: ______R1__ (IDENSDR FDEA201911263098Tee Fitting · corrodedFORWARD CARGO DOOR LOWER INTERCOSTAL OUTER TEE #4 FROM FWD SIDE IS CORRODED EVALUATED CORROSION ON FWD CARGO DOOR LWR. INTERCOSTAL OUTER TEE #4 FROM FWD SIDE FOUND TO BE 100% OUT OF LIMITS IAW B757 SRM 53-30-02-1A FIG. 101 DET. IV, REMOVED OUTER SUPPORT TSDR FDEA2019112653091Floor Panel · delaminatedFLOOR PANEL AT DOOR 1L DAMAGED REPAIRED FLOOR PANEL AT DOOR 1L IAW SRM 53-00-50-2RSDR FDEA2019112643084Beam · corrodedTRANSVERSE BEAM B/S 1040-1075, RBL 25 IS CORRODED BEYOND LIMITS IAW SRM 53-00-51-1A ,ALLOWABLE DAMAGE 1, DETAIL III. REPLACED TRANSVERSE BEAM IAW SRM 51-40-02 AND BOEING DRAWING #114N8250.SDR FDEA2019112643083Beam · corrodedTRANSVERSE BEAM B/S 1040-1075 RBL 46 IS CORRODED BEYOND LIMITS IAW SRM 53-00-51-1A, ALLOWABLE DAMAGE 1, DETAIL III. INSTALLED NEW TRANSVERSE BEAM IAW SRM 51-40-02 AND BOEING DRAWING # 144N8250SDR FDEA201911243082Beam · corrodedTRANSVERSE BEAM B/S 1040-1075, LBL 25 IS CORRODED BEYOND LIMITS IAW SRM 53-00-51-1A, ALLOWABLE DAMAGE 1, FIG 101, DETAIL III REPLACED BEAM IAW SRM 51-40-02 AND BOEING DRAWING#144N8250SDR FDEA2019112633062Beam · corrodedTRANSVERSE BEAM AT B/S 1040-1075 LBL 46 HAS CORROSION BEYOND PERMITTED LIMITS IAW SRM 53-00-51-1A ALLOWABLE DAMAGE 1 DETAIL III. REPLACED CORRODED BEAM IAW SRM 51-40-02 AND DRAWING 144N8250.SDR FDEA2019112633064Floor Panel · gougedNUMEROUS DENTS AND GOUGES FOUND AT AFT CARGO FLOOR PANEL LOCATED BETWEEN BS 1330 AND BS 1470 REPLACED AFT CARGO COMPARTMENT FLOOR PANEL IAW BOEING DRAWING #453N1805, PN 453N1805-176.SDR FDEA2019112633063Floor Panel · gougedNUMEROUS DENTS AND GOUGES FOUND AT AFT CARGO FLOOR PANEL LOCATED BETWEEN BS 1200 AND BS 1330 APPROX. REPLACED AFT CARGO COMPARTMENT FLOOR PANEL IAW BOEING DRAWING # 453N1805. PN.453N1805 -137SDR FDEA201911223038Seat Track · corrodedSEAT TRACK CORRODED BEYOND PERMITTED LIMITS IAW SRM 53-00-52-1A ALLOWABLE DAMAGE 1 FIG 101 DETAIL VII. REPLACED SEAT TRACK IAW SRM 51-40-02 AND DRAWING 144N5001.SDR FDEA201911223037Seat Track · corrodedSEAT TRACK CORRODED BEYOND LIMITS AT BS 1075-1180 RBL 46 IAW SRM 53-00-52-1A ALLOWABLE DAMAGE 1, FIG 101, DETAIL VII. REPLACED SET TRACK IAW SRM 51-40-02 AND DRAWING 144N5001.SDR FDEA201911223043Floor Panel · delaminatedFLOOR PANEL DAMAGED UNDER FWD LAV REPAIRED FLOOR PANEL IAW SRM 53-00-50-2RSDR FDEA2019112202998Outflow Valve · inoperativePDIS 921 21-30 8717 20NOV19 MEM FACT U LOGPAGES:3170064 SAME PROBLEM AS YESTERDAY WITH PRESSURIZATION EXCEPT AUTO 1, AUTO 2 AND MANUAL CONTROL WORKED. HOWEVER THE PRESSURIZATION OF THE AIRCRAFT COULD NOT KEEP UP ABOVE FL 250. CABIN PRESSURE CSDR FDEA201911192993Outflow Valve · failedPDIS 921 21-30 8714 19NOV19 MCI OPEN U LOGPAGES:3170061 CABIN AUTOMATIC INOP. UNABLE TO MAINTAIN CABIN ALT IN MANUAL WITH VALVE FULLY CLOSED. REPLACED CABIN PRESSURE OUTFLOW VALVE AND TESTED PER AMM 21-31-03SDR FDEA201911192997Controller · failedCABIN AUTOMATIC INOP. UNABLE TO MAINTAIN CABIN ALT IN MANUAL WITH VALVE FULLY CLOSED. REPLACED CABIN PRESSURE OUTFLOW VALVE AND TESTED PER AMM 21-31-03-2, OPS CHECKS GOOD. REPLACED #2 AUTOMATIC PRESSURE CONTROLLERSDR FDEA201911192994Bracket · cracked#10 LE SLAT INBOARD MAIN TRACK LOWER BRACKET CRACKED. BRACKET REPLACED IAW SRM 51-40-02 AND BOEING DRAWING #114N4002SDR FDEA201911192992Support Angle · crackedAPU DUCT SUPPORT ANGLE CRACKED AND BRACKETS AT BS 1781 WORN APU DUCT SUPPORT ANGLE AND BRACKETS AT BS 1791 REPLACED IAW SRM 51-40-02SDR FDEA2019120413166Support Angle · corrodedAPU INLET PANEL SUPPORT ANGLE HAS EVIDENCE OF CORROSION AT ANCHOR NUT ATTACH POINT LOCATED AT BS 1790 S6R CORROSION REMOVED IAW SRM 51-10-02 AND FOUND TO BE OUTSIDE LIMITS IAW SRM 53-00-04- 1A ORIGINAL MATERIAL THICKNESS = 0.063" REMOVED MATERIAL = 0.030". SDR FDEA2019120433165Angle · corrodedUPON REMOVAL OF APU INLET, CORROSION FOUND ON UPPER AND LOWER ANGLES REMOVED CORROSION IAW SRM 51-10-02 AND FOUND TO BE OUTSIDE LIMITS IAW 53-00-04-1A ORIGINAL MATERIAL THICKNESS = 0.063" REMOVED MATERIAL = 0.032" UPPER AND LOWER ANGLES REPLACED IAW SRSDR FDEA2019120133156Strap · corrodedUPON REMOVAL OF APU INLET CORROSION FOUND ON STRAP AT BSTA 1825. CORROSION REMOVED IAW SRM 51-10-02 AND ONE AREA FOUND TO BE OUTSIDE LIMITS IAW SRM 53-80-15-1A AT MIDDLE STRAP AREA. CARRIED OUT SINGLE STRAP REPAIR IAW SRM 53-80-15-2R REPAIR 2.SDR FDEA2019111522934Battery · smokeSTRONG BURNING ELECTRICAL SMELL MAIN CARGO COMPARTMENT T/S FOUND APU BATTERY SMOKING WITH A HEAVY BURNT SMELL. R&R APU BATTERY REF AMM 24-31-03-4. ALSO R&R APU BATTERY CHARGER REF AMM 24-31-04-4 PRECAUTIONARY. OPS CK'D GOOD. A/C OK FOR SERVICESDR FDEA2019112683065Floor Panel · damagedNUMEROUS DENTS AND GOUGES FOUND AT AFT. CARGO FLOOR PANEL, LOCATED BETWEEN FWD EDGE AND BSTA 1330 APPROX REPLACED AFT CARGO COMPARTMENT FLOOR PANEL IAW BOEING DRAWING # 453N1805 PN 453N1805 - 137.SDR FDEA201912133237Structure · corrodedCORROSION AT BS 900 LBL 8 AND RBL 8 WL 138 CORROSION. REMOVED AT B/S 900 LBL 8 AND RBL 8 WL 138 IAW SRM 53-00-71-1A AND FOUND TO BE OUTSIDE SRM LIMITS. AREA REPAIRED IAW EA F-5300-T0351157 P1.SDR FDEA2019110973201Seat Track · corrodedSEAT TRACK BSTA 900-1180 LBL 58 HAS CORROSION. SEAT TRACK REPLACED IAW EA F-5321-T0351032 P1 AND DRAWING 657N3321.SDR FDEA201911073200Seat Track · corrodedSEAT TRACK BSTA 900-1180 RBL 58 HAS CORROSION. REPLACED SEAT TRACK SECTION BS 900 TO BS 1180 RBL 58, IAW EA F-5321-T0351032 P1 AND DRAWING 657N3321.SDR FDEA2019120973199Seat Track · corrodedSEAT TRACK BSTA 1180-1200 RBL 46 CORROSION CORROSION REMOVED AND EVALUATED IAW SRM 53-00-52-1A AND FOUND TO BE OUTSIDE SRM LIMITS SEAT TRACK SECTION REPAIRED IAW SRM 53-00-52-2R REPAIR 3 OPTION 2 AND FEDEX EA # F- 5300-TO351197SDR FDEA2019120963206Support Bracket · crackedEVIDENCE OF CRACKS AT ACCESS PANEL 313AL BOTH STOP SUPPORT BRACKETS REMOVED ACCESS PANEL 313AL STOP SUPPORT ASSEMBLYS L/H AND R/H SIDES. REPLACED STOP SUPPORT ASSEMBLY BRACKETS ( GUSSETS) PN .148N6614-7, 148N6614-8 ,148N6614-9 AND 1486614-10 IAW SRM 51-4SDR FDEA201912093211Attach Bracket · corrodedEVIDENCE OF CORROSION FOUND AT L/H ELEVATOR OUT/BONDING JUMPER ATTACH BRACKET REPLACED CORRODED BRACKET IAW SRM 51-40-02 AND BOEING DRAWING #183N1703 AT L/H HORIZONTAL STABILIZER UPPER TE OUTBOARD END.SDR FDEA2019110653198Floor Support · wornQTY 5 OPEN HOLES ON MAIN CARGO DECK FLOOR STRUCTURE SUPPORT FRAME BETWEEN B.STA 1480-1500 RBL 29 REMOVED UPPER ANGLE IAW SRM 51-4-02 REPLACED UPPER ANGLE IAW SRM 51-40-02, BOEING DRAWING # 284N1796 AND FEDEX GMM 7- 0-1001,SDR FDEA2019111952987Seat Track · corrodedEVIDENCE OF CORROSION ON SEAT TRACK MAIN DECK AREA BS 344-BS365 , LBL 6.75 CORROSION FOUND TO BE OUTSIDE LIMITS IAW SRM 55-00-52-1A, SEAT TRACK REPLACED IAW VENTURA AEROSPACE DRAWING # 3504 AND SRM 51-40-02.SDR FDEA201912043174Beam · damagedDRILL MARK ON BEAM LWR FWD FLANGE FROM BS 720 RBK 66 ST17 REPAIR CARRIED OUT IAW FEDEX EA # F- 5310-T0351050. PART 1 (P1) TITLE : FUSELAGE - MAINFRAME-DRILL MARK FLOOR BEAM BS 720 RBL 66SDR FDEA2019120413160Skin · corrodedR/H IWNG OVERWING FILL PART FAILED BONDING CHECK R/H MAIN FUEL TANK OVERWING FILL PORT REMOVED IAW AMM 28-11-04 AND EVIDENCE OF CORROSION FOUND. REPAIR CARRIED OUT IAW FEDEX EA #F-5730-T0350826 P1 TITLE : RH WING - PLATES & SKINS - OVERWING FILL PORT - COSDR FDEA2019120433159Skin · corrodedL/H WING OVERWING FILL PORT FAILED BONDING CHECK L/H MAIN FUEL TANK OVERWING FILL PORT REMOVED IAW AMM 28-11-04 AND EVIDENCE OF CORROSION FOUND. REPAIR CARRIED OUT IAW FEDEX EA # F-5730-T0350814 P1 TITLE: L/H WING - PLATES & SKINS - OVERWING FILL PORT - C
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