Boeing 757-222
Service difficulty reports · 15,539
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 = '757222' 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 = '757222' 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 FDEA202011252970Floorbeam · corrodedMAIN CABIN FLOOR BEAM LOWER SURFACE IS CORRODED UNDER NUT PLATE BS 1681, LBL 39.5. REPLACED NUT PLATE STRIP AS REQUIRED, IAW BOEING DRAWINGS 146N5693 REV "B", 146N5300 REV "F", AND B757 SRM 51-40-02.SDR FDEA202011252969Floorbeam · corrodedMAIN CABIN FLOOR BEAM LOWER SURFACE IS CORRODED UNDER NUT PLATE BS 1681, LBL 32. REPLACED NUT PLATE STRIP AS REQUIRED, IAW BOEING DRAWINGS 146N5693 REV "B", 146N5300 REV "F", AND B757 SRM 51-40-02.SDR FDEA202011252968Floorbeam · corrodedMAIN CABIN FLOOR BEAM LOWER SURFACE IS CORRODED UNDER NUT PLATE BS 1681-RBL 18. REPLACED NUTPLATE AS REQUIRED, IAW BOEING DRAWINGS 146N5693 REV "B", 146N5300 REV"F", AND B757 SRM 51-40-02.SDR FDEA202011252967Floorbeam · corrodedMAIN CABIN FLOOR BEAM LOWER SURFACE IS CORRODED UNDER NUTPLATE BS 1681-RBL 12. REPLACED NUTPLATE STRIP AS REQUIRED, IAW BOEING DRAWINGS 146N5693 REV "B", 146N5300 REV "F", AND B757 SRM 51-40-02.SDR FDEA202011252966Floorbeam · corrodedMAIN CABIN FLOOR BEAM LOWER SURFACE IS CORRODED UNDER NUT PLATE AT PRESSURE DECK THRU AFT PIT BULKHEAD PANEL BS 1681-RBL 36. REPLACED NUTPLATE STRIP AS REQUIRED, IAW BOEING DRAWINGS 146N5693 REV "B", 146N5300 "F", AND B757 SRM 51-40-02.SDR FDEA202011242962Floorbeam · corrodedMAIN CABIN FLOOR BEAM LOWER SURFACE IS CORRODED UNDER NUTPLATE BS 1681-RBL 24. REPLACED NUTPLATE STRIP AS REQUIRED, IAW BOEING DRAWINGS 146N5693 REV "B", 146N5300 REV "F" AND B757SRM 51-40-02.SDR FDEA202011242961Floorbeam · corrodedMAIN CABIN FLOOR BEAM LOWER SURFACE IS CORRODED UNDER NUTPLATE BS 1681-RBL 4. REPLACED NUTPLATE STRIP AS REQUIRED, IAW BOEING DRAWINGS 146N 5693 REV "B", 146N5300 REV "F", AND B757 SRM 51-40-02.SDR FDEA202011242960Floorbeam · corrodedMAIN CABIN FLOOR BEAM UPPER SURFACE IS CORRODED AT FASTENER HOLE BS 1681, LBL 24-BL 47. REMOVED SURFACE CORROSION AS REQUIRED, IAW B757 SRM 53-60-51-1A. ORIGINAL MATERIAL THICKNESS .071. MATERIAL LOSS .006. REMAINING MATERIAL THICKNESS .065 FOUND TO BE WISDR FDEA202011242959Floorbeam · corrodedMAIN CABIN FLOOR BEAM UPPER SURFACE IS CORRODED AT FASTENER HOLE BS 1681, BL 4-RBL 54. REMOVED SURFACE CORROSION AS REQUIRED, IAW B757 SRM 53-60-51-1A. ORIGINAL MATERIAL THICKNESS .071, MATERIAL LOSS .004 REMAINING MATERIAL THICKNESS .067 FOUND TO BE WITHIN SDR FDEA202011242957Structure · damagedG1A GALLEY LOWER INBOARD DOOR TRIM DAMAGED AT LOWER INBOARD CORNER. ACCOMPLISHED FEDEX EA F-2530-T0358223-P1 EQUIP AND FURNISH-GALLEY-ICE CHEST DOOR TRIM-DAMAGED.SDR FDEA202011232947Frame · crackedSTA 1640 FUSELAGE FRAME WEB AND STR-14L INTERCOSTAL TEE CLIP. LOWER INBOARD HOLE HAS (2) CRACK INDICATIONS AT 3 AND 9 O`CLOCK POSITIONS. LOWER OUTBOARD HOLE HAS (1) CRACK INDICATION AT 3 TO 4 O`CLOCK POSITION. ALL WORK ACCOMPLISHED, IAW FEDEX EA F-5310-T035SDR FDEA202011192910Skin · delaminatedDISBOND UPPER SURFACE RIGHT INBOARD MAIN FLAP REPAIRD UPPER SURFACE OF RT INBOARD MAIN FLAP, IAW B757 SRM 51-70-10-2R REP 2 AND 57-50-01 01-2R REP 1.SDR FDEA202011142855Actuator · twistedPER CREW DEBRIEF, MEM RAMP HAD DIFFICULTY IN CLOSING MCD. MX CALLED TO A/C TO CLOSE MCD, STATED MCD OUT OF SEQUENCE. MCD DOOR OPENED NORMALLY AT GSP. WHEN CLOSING MCD, FOUND BOTH DOOR ACTUATORS TWISTED IN SUPPORT BRACKET, FOUND 4 EACH MCD SUPPORT ROD ENDS SDR FDEA202011142854Lamp · inoperativeL-1 EXTERIOR EMERGENCY EXIT LIGHT INOPERABLE ON TEST. RELAMPED L 1 DOOR SLIDE LIGHT, PER B757-200 AMM 33-51-06-2-1. OPERATIONS CHECKS NORMAL.SDR FDEA202011132838Structure · brokenRT WING NR 8 NSLAT LOWER CORNER BROKEN, MISSING CORNER. REPAIRED IAW B757 SRM 57-43-01-2R AND SRM 51-70-07-0G.SDR FDEA202011082798Floor Support · corrodedMAIN CABIN FLOORBOARD INTERCOSTAL IS CORRODED AT 2 FASTENER HOLES BS 1689-BS 1695 BL 0. REMOVED AND REPLACED INTERCOSTAL AND INTERCOSTAL STRAP, IAW B757 SRM 51-40-02, BOEING DWG: 146N5230 REV: -, B757 SRM 51-20-01.SDR FDEA202011072787Skin · corrodedEXTERIOR FUSELAGE SKIN HAS EVIDENCE OF CORROSION AND BULGED SKIN AT SPLICE ARE BS 1455-BS 1462 STR 30-STR 28R. REMOVED FASTENERS AT STA 1459 STR 28R TO 28L AND 1 EA SHEAR TIE AT STA 1459 STR 30-29R, IAW B757 SRM 51-40-02. REMOVED 1 EA SHEAR TIE STA 1459 STR SDR FDEA202011062786Panel · debondedE&E COMPARTMENT AFT OF NOSE GEAR THE P32 PANEL RIGHT DOOR UPPER RIGHT CORNER IS DISBONDED. REMOVED EDGE DAMAGE, IAW EA F-2500-T0357818 P1 FIG1, MATERIAL ID FOR ADHESIVE BMS5-92 TY1, IAW EA F-2500-T0357818 P1 & B757-200 SRM 51-70-10-2R REPAIR 1 PARA 3D. MIXEDSDR FDEA202011052785Seat Track · corrodedMAIN CABIN SUPERNUMERARY LT SEAT TRACK UPPER SURFACE CORRODED MAIN CABIN SUPERNUMERARY LT SEAT TRACK CORROSION FOUND TO BE OUT OF LIMITS, IAW B757 SRM 53-00-52-1A FIGURE 101 DETAIL 1. REMOVED SEAT TRACK, IAW B757 SRM 51-40-02. FABRICATED NEW SEAT TRACK, IAWSDR FDEA202011052784Rub Strip · crackedR1 DOOR OPENING CENTER GUIDE FITTING RUBSTRIP IS CRACKED. REPLACED CENTERING GUIDE, IAW B757 SRM 51-40-02-0G AND DWG 141N8412 REV G.SDR FDEA202011052774Door · corrodedBELOW L2 DOOR THE LAV SERVICE DOOR DOUBLER IS CORRODED. REMOVED CORROSION, IAW B757 CPM 20-40-00, MATERIAL REMOVED .002 FROM .071, EVALUATED AREA FOUND TO BE LESS THAN 10% WITHIN LIMITS, IAW B757 SRM 53-00-01-1A. ALODINED AREA, IAW B757 SRM 51-20-01-OG. PRISDR FDEA202011042773Skin · corrodedEXTERIOR FUSELAGE UPPER ADF ANTENNA AREA STA 1116 HAS LIGHT PITTING. REMOVED CORROSION PITTING ORIGINAL MATERIAL .110, REMOVED .010, .100 REMAINING FOUND TO BE WITHIN LIMITS, IAW B757 SRM 53-00-01-1A. APPLIED CLEAR 1001 ALODINE, IAW B757 AMM 51-21-04-7.SDR FDEA202011042771Hinge · corrodedG1A GALLEY COMPARTMENT 102 DOOR HINGE CORRODED. ACCOMPLISHED FEDEX EA MF-2530-T0357769 EQUIP AND FURNISH G1A GALLEY DOOR HINGE, CORROSION DAMAGE.SDR FDEA202011032763Skin · damagedRT WING FIXED LEADING EDGE SKIN UPPER SURFACE HAS FASTENERS PULING THROUGH APPROXIMATELY 2' OUTBOARD OF THE PYLON. REMOVED LEADING EDGE SKIN AND ACCOMPLISHED SRM REPAIR 57-41-01-2R, REINSTALLED REPAIRED SKIN.SDR FDEA202011032762Skin · delaminatedRT WING FIXED LEADING EDGE SKIN UPPER SURFACE IS DELAMINATED APPROXIMATELY 2.5' OUTBOARD OF THE PYLON. REMOVED LEADING EDGE SKIN AND ACCOMPLISHED SRM REPAIR 57-41-01-2R, REINSTALLED REPAIRED SKIN.SDR FDEA202011032760Panel · dentedVERTICAL STAB LEFT SIDE PANEL 322DL HAS DENT REPAIRED VERTICAL STABILIZER LEFT SIDE PANEL 322DL BY BONDING REPAIR PLIES, IAW B757 SRM 55-30-01-0I FIG 1 AND 55-30-01-2R REPAIR 4 FIG 201 AND 51-70-06 PARA 5 A FIGURE 5 AND REPAIR GENERAL. APPLIED FINISH, IAW B7SDR FDEA202010312733Support Angle · crackedNR 2 PYLON UNDER PANEL NR 445CL SUPPORT ANGLE IS CRACK AT NAC 204 APPROXIMATELY. REMOVED AND REPLACED SUPPORT ANGLE AT NR 2 PYLON, IAW FEDEX B757 DWG 313N3052 REV B AND SRM 51-40-02-0G.SDR FDEA202010312732Skin · dentedLEFT HORIZONTAL STABILIZER LOWER SKIN BETWEEN AUX SPAR AND FRONT SPAR HAS A DENT. REPAIRED DENT, IAW B757 SRM 55-10-01-1A AND 51-70-10-2R.SDR FDEA202010302722Gust Lock · failedR1 ENTRY DOOR GUST LOCK COLLAR CRACKED/BROKEN. REPLACED BROKEN R1 DOOR HOLD-OPEN LOCK COLLAR WITH A NEW SPLIT COLLAR AND CATCH, REF B757 AMM 52-11-08-8. ALLIANCE AEROSPACE ENGINEERING KIT PN 10-N0244-8 CONTAINS 10-N6008-4 (LOT 22457 SN 12-0010) 10-N6009-1 (LSDR FDEA202010302720Plate · crackedRT WING,OUTBOARD FLAP TRACK FAIRING 673CB SPACER PLATE IS CRACKED LOCATED ON TOP OF THE INBOARD BLADE SEAL RETAINER STRIP. REMOVED AND REPLACED SPACER PLATE AT RT WING OUTBOARD FLAP INBOARD TRACK FAIRING 673CB, IAW FEDEX B757 DWG 113N3131 REV A.SDR FDEA202010292712Bracket · crackedNR 1 ENGINE, INBOARD CORE COWL, LOWER FORWARD BRACKET CRACKED. REMOVED AND REPLACED BRACKET, PER DWG 314N3210 REV H AND B757 SRM 51-40-02.SDR FDEA202010292702Transmission · tripped"TRAILING EDGE FLAP DISAGREE" EICAS ILLUMINATED WHEN FLAP HANDLE MOVED FROM FLAP 20 TO FLAP 25 DETENT ON SHORT FINAL. PERFORM GO AROUND. FLAP HANDLE MOVED TO 20 DURING GA, RAN QRH. NO ASYMMETRY. NO UNUSUAL ROLLING MOTIONS. FLAPS INDICATED APPROXIMATELY 22 SDR FDEA202010252651Floorboard · corrodedMAIN CABIN FLOOR BOARD STRUCTURE IS CORRODED AT 2 FASTENER HOLES BS 1688.5-BS 1695 RBL 56. REMOVED 3 EA NUTPLATES. BLENDED AREA FREE OF CORROSION. ORIG MATERIAL .071 REMOVED .008 REMAINING .063 WITHIN LIMITS, IAW B757 SRM 53-60-15 AND 51-10-02. ALODINED ASDR FDEA202010232629Seat Track · corrodedCORROSION ON SEAT TRACK COURIER AREA STA 370 LBL 8. REMOVED AND REPLACED BY FABRICATION SEAT TRACK AT STA 345 TO STA 377 LBL 8, IAW B757 SRM 51-40-02-0G, 51-20-01-0G AND VERNTURA AEROSPACE DWG 3470 REV G AND DCN 3504-NC-1.SDR FDEA202010232628Skin · dentedSKIN PROTRUSION FOUND EXTERIOR LT LOWER LOBE BS 520 EVALUATED DENT ON FUSELAGE SKIN AT STA 522 STR 26L TO 27L FOUND BETWEEN 3 INCHES FROM SKIN SPLICE AND TO BE OUT LIMITS, IAW B757 SRM 53-00-01-1A FIG 101 DETAIL III. CUT OUT DAMAGED SKIN AREA. FABRICATED, LOSDR FDEA202010232627Floorbeam · crackedMAIN DECK STA 1050 RBL 38 FLOOR SUPPORT CRACKED AFTER REMOVAL OF TOP PLATE AND FURTHER EVALUATION NO DAMAGE FOUND AT FLOOR SUPPORT STA 1050 RBL 24 TO RBL 44. DAMAGE ONLY ON TOP PLATE, IAW B757 SRM 51-10-02. FABRICATED AND INSTALLED NEW TOP PLATE AT STA 1050 SDR FDEA202010222603Skin · crackedAIRCRAFT DAMAGED STA 1620 UNDER STR 17L DENT IS L=1.75" W=1". C/W EA NR F-5330-T0357572 P1 TITLE: FUSELAGE-PLATES AND SKIN-FUSELAGES SKIN REPAIR NEAR STA 1620 BETWEEN STRINGERS S-16L AND S-18L.SDR FDEA202010192557Paint · deterioratedNR 1 PYLON AFT FIXED INBOARD SIDE ABOVE EXHAUST NOZZLE HAS PAINT DETERIORATED AND EVIDENCE OF CORROSION. REPAIRED AFT FAIRING SKIN, IAW B757-200 SRM 54-51-70-01 AND 54-51-70-2R REPAIR 4.SDR FDEA202010192558Structure · damagedCUSTOMER REQUEST, EVALUATE FASTENER SPACING ON ATTACHMENT ANGLE AT BL 0 FWD OF FRAME AT STA 231.25. REMOVED AND REPLACED CHORD AND INTERCOSTAL, PER DWG 141N8222 AND EA F-5310-T0357422. TITLE;FUSELAGE-MAINFRAME-INTERCOSTAL, STA 273 TO 231, BL 0.SDR FDEA202010162534Idg · failedRT GEN OFF IN FLIGHT. CREW RAN QRH AS REQUIRED. CHECKED ELEC/HYD DISPLAY SELECT SWITCH ON THE EICAS PANEL AT P61 HAD RT GEN DRIVE PUSH THE BIT SWITCH ON THE BUS POWER CONTROL UNIT MESSAGES WAS RT LOW OIL AND DELTA TEMP OPENED COWL AND FOUND DELTA P POP ON RISDR FDEA202010162532Skin · dentedRT RUDDER SKIN HAS A DENT BETWEEN RUDDER STA 231.852 AND 306.371 AND APPROXIMATELY 33" INCHES FROM THE TRAILING EDGE. MARKED REPAIRED DENT ON RT RUDDER SKIN, IAW B757 SRM 55-40-01-2R AND 51-70-03 PARA 5 L.SDR FDEA202010162530Structure · delaminatedNR 1 ENGINE INBOARD FAN COWL HAS LARGE AREA OF EXPOSED COMPOSITE MATERIAL. REMOVED AND REPLACED INBOARD FAN COWL, IAW B757 AMM 7-1-11-04-4.SDR FDEA202010152515Frame · crackedHOLE AT STA 1640LH BELOW STR 14L HAS CRACK INDICATION. ACCOMPLISHED EA F-5310-T0357159: FUSELAGE-MAINFRAME-FRAME STA 1640 S-14L CRACK INDICATION. THIS EA DEVIATES FROM EO F-5310-E0344602.SDR FDEA202010152514Strap · corrodedNUTPLATE STRAP CORRODED AT STA 1721 LEFT SIDE ABOVE PNEUMATIC DUCT. REMOVED AND REPLACED NUTPLATE STRAPS, IAW B757 SRM 51-40-02 B757 SRM 51-20-01, BOEING DWG: 146N5693 REV: B. ACCOMPLISHED EA: F-5321-T0357460-P1 FUSELAGE-CARGO COMP FLOORS -FLOOR SUPPORT, STSDR FDEA202010132484Shoulder Belt · twistedPDIS 770 25-10 4970 13OCT20 MEM FACT U. CA SHOULDER HARNESS WILL NOT RETRACT. FACT 13OCT20 18:15 MEM U. FOUND CA HARNESS TWISTED. UNTWISTED HARNESS AND OPERATIONS CHECK, PER 757 M/M 25-11-00-6. OPERATIONS CHECK NORMAL.SDR FDEA202010132483Nut Plate · corrodedNUTPLATE STRAP AND NUTPLATE ARE CORRODED ON FLOORBEAM BS 1681.8 LBL 24. REMOVED CORROSION, IAW B757 SRM 53-00-51-1A AND REPLACED NUTPLATE STRAP, IAW BOEING DWG 146N5693 REV B.SDR FDEA202010132482Nut Plate · corrodedNUTPLATE STRAP AND NUTPLATE ARE CORRODED 2 PLACES LEFT SIDE ABOVE PNEUMATIC DUCT BS 1681.8. REMOVED CORROSION, IAW B757 SRM 53-00-51-1A. REPLACED NUTPLATE STRAP, IAW DWG 146N5693 REV B.SDR FDEA202010122463Panel · crackedPARTS RACK, LT WING FLAP FAIRING PANEL 574ER IS CRACKED. RECEIVED NEW PANEL (574ER) P/N 113N1712U4, PER B757 IPC 27-51-31-03.SDR FDEA202010102459Frame · crackedLT BS 1640 FRAME LEWER INBOARD HOLE HAS (2) INDICATIONS OF CRACKS AT 3 O`CLOCK AND 9 O`CLOCK POSITIONS. C/W FEDEX EA NR F-5310-T 0357202 P1 TITLE: FUSELAGE-MAINFRAME-STA 1640 SPLICE REPAIR BETWEEN STRINGER I-9 F AND S-20L.SDR FDEA202010082442Bottle · defectiveR1 DOOR POWER ASSIST HAS LOW PRESSURE. REMOVED DEFECTIVE BOTTLE AND INSTALLED NEW PART.
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