N791FD

Service difficulty reports · 97

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N791FD' AND registry_match = 'registration'
  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.

SDR FDEA202202210342None · noneMAIN CABIN FLOORBEAM UPPER CAP NUTPLATE STRAP HAS CORROSION ON LOWER SURFACE AR STA 1682 LBL 40 REMOVED, FABRICATED AND REPLACED NUTPLATE STRAP IAW BOEING DWG 146N5693 REV B, SRM 51-10-02-0G, 51-20-01-0GFeb 21, 2022 · N791FD · Boeing 757200 · Fuselage Miscellaneous StructureSDR FDEA202202210340None · noneMAIN CABIN LH SIDE FLOOR WEB LOWER STIFFENER HAS CORROSION ON LOWER SURFACE AT 1EA NUTPLATE LOCATION AT APPROX STA 1680 LBL 55 REMOVED CORROSION AS REQUIRED LH FLOOR WEB STIFFENER LOWER SURFACE, REMAINING MATERIAL IS .064", REMOVED .006", ORIGINAL .070" FFeb 21, 2022 · N791FD · Boeing 757200 · Fuselage Miscellaneous StructureSDR FDEA202202210339None · noneMAIN CABIN LH SIDE FLOOR WEB HAS CORROSION ON UPPER AND LOWER SURFACE AT NUTPLATES LOCATIONS FROM STA 1640 - 1682 LBL 55 REMOVED CORROSION AS REQUIRED ON UPPER AND LOWER SURFACES, REMAINING MATERIAL IS .064", REMOVED .007", ORIGINAL .071" FOUND TO BE WITHFeb 21, 2022 · N791FD · Boeing 757200 · Fuselage Miscellaneous StructureSDR FDEA202202210337None · noneMAIN CABIN RH SIDE FLOOR WEB LOWER STIFFENER HAS CORROSION ON LOWER SURFACE AT NUTPLATE LOCATIONS FROM STA 1640-1664 RBL 55 REMOVED CORROSION AS REQUIRED ON LOWER STIFFENER SURFACE, REMAINING MATERIAL IS .064", REMOVED .006", ORIGINAL .070" FOUND TO BE WIFeb 21, 2022 · N791FD · Boeing 757200 · Fuselage Miscellaneous StructureSDR FDEA202202210336None · noneMAIN CABIN RH SIDE FLOOR WEB HAS CORROSION ON UPPER AND LOWER SURFACES AT NUTPLATE LOCATIONS FROM STA 1640-1682 RBL 55 REMOVED CORROSION AS REQUIRED ON UPPER AND LOWER SURFACES, REMAINING MATERIAL IS .065", REMOVED .006", ORIGINAL .071" FOUND TO BE WITHINFeb 21, 2022 · N791FD · Boeing 757200 · Fuselage Miscellaneous StructureSDR FDEA202202210346Rub Strip · cracked#2 PYLON HYDRO BAY DOOR OPENING AFT STRIKER PLATE IS CRACKED REMOVED AND REPLACED PER BAC DWG # 313N3053 REV EFeb 21, 2022 · N791FD · Boeing 757200 · Nacelle/Pylon StructureSDR FDEA202202210345Seal · cracked#2 ENG UPPER I/B SIDE OF EXHAUST DUCT SPRING SEAL IS CRACKED REMOVED AND REPLACED SPRING SEAL PER BAC DWG # 314N3310 REV FFeb 21, 2022 · N791FD · Boeing 757200 · Engine Exhaust SystemSDR FDEA202202210343None · noneMAIN CABIN AFT DECK PLATE UPPER SURFACE STA 1681 LBL 20 TO 55 FLOORBOARD ATTACHMENT HOLES DAMAGED. ACCOMPLISHED FEDEX EA# F-5310-T0367139 FUSELAGE - MAINFRAME- FLOOR BEAM AND DECK PLATE - STA 1681 - LBL 32 - 47, ELONGATED HOLESFeb 21, 2022 · N791FD · Boeing 757200 · Fuselage Main, StructureSDR FDEA202202190323None · noneM AIN CARGO SEAT TRACK SURFACE WORN BS 700 RBL 24 REMOVED AND REPLACED SEAT TRACK IAW B757-2 SRM 51-40-02-0G AND DWG 143N5080 REV B, ACCOMPLISHED FEDEX EA # F-5310-T0367159-P1, FUSELAGE - MAINFRAME - SEAT TRACK, STA 700-780 RBL 24, ALTERNATE FINISHFeb 19, 2022 · N791FD · Boeing 757200 · Fuselage Main, StructureSDR FDEA202109042212Controller · malfunctionedPDIS 791 21-30 4670 04SEP21 CPR OPEN U CABIN ALTITUDE WARNING OCCURRED AT CRUISE FL 390 WITH CABIN ALTITUDE CONTROL IN AUTO 2. BEGAN AN IMMEDIATE EMERGENCY DESCENT TO 16,000 WHILE RUNNING QRC AND QRH CHECKLISTS. CABIN ALTITUDE SEEMED TO COME Sep 4, 2021 · N791FD · Boeing 757222 · Cabin Pressure ControllerSDR FDEA202104080845Flap System · unknownAFTER TAKEOFF IN MODERATE TURBULENCE FLAPS 5 LIMIT SPEED (210 ITS)EXCEEDED. SPEED REACHED 213 ITS FOR 3 SECONDS WHILE FLAPS IN TRANSIT TO FLAPS 1. PERFORMED PHASE 1 INSPECTION REF B 757 AMM 05-51-08-2. NO DEFECTS NOTED A/C OK FOR SERVICE.Apr 8, 2021 · N791FD · Boeing 757222 · Trailing Edge FlapsSDR FDEA202101050009Controller · failedUPON STARTING SECOND ENGINE GOT A "AFT CABIN TEMP", FWD CABIN TEMP" FLT DECK TEMP" EICAS WARNING MESSAGES. ACCOMPLISHED CHECKLIST/SHUT DOWN. FOUND ZONE TEMP CONTROLLER (GARRETT) PN 625934-6, SERIAL 071C-126 FAULTED. REMOVED AND REPLACED ZONE TEMP. CONTROLLJan 5, 2021 · N791FD · Boeing 757222 · Cabin Temperature Control SystemSDR FDEA202002240381Strap · damagedAFT. CARGO COMPT. AFT. BULKHEAD BETWEEN BS.1681, AND BS. 1701, INTERCOSTAL WEB LOWER FLANGE HAS 26EA. DRILL OFF RIVETS SHANKS, AND MISSING STRAP, AT BL0. FORMED, LOCATED, DRILLED, FABRICATED AND INSTALLED AFT CARGO STA 1681-1701 BL0 INTERCOSTAL WEB LWR FLFeb 24, 2020 · N791FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA202002240380Intercostal · damagedAFT. CARGO COMPT. AFT. BULKHEAD INTERCOSTAL LOWER FLANGE HAS 1EA. DAMAGED FASTENER HOLE, AT BL0 BETWEEN BS. 1681, AND BS.1701 EVALUATED INTERCOSTAL LWR FLANGE (CHANNEL) BL0 STA 1681-1701 OUT OF LIMITS IAW B757 SRM 51-10-02 AND 53-00-04-1A FIG 101. REMOVEFeb 24, 2020 · N791FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA202002210364Seat Track · corrodedSEAT TRACK AT STA 1180 LBL45.5 HAS CORROSION REMOVED CORR ON SEAT TRACK STA 1180 LBL45.5 IAW B757 SRM 51-10-02. 100% MAT LOSS DUE TO EXFOILIATION OUT OF LIMITS IAW B757 SRM 53-60-52-1A FIG 101. REMOVE, F FABRICATED AND INSTALLED NEW SEAT TRACK IAW B757 SFeb 21, 2020 · N791FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201803260784Shutoff Valve · failedLEFT ENGINE BLEED PRESSURE FLUCTUATED BETWEEN 0 AND 40 PSI. LOST CABIN PRESSURIZATION, RECEIVED A CABIN ALTTITUDE WARNING. RAN QRH , DESCENDED TO 1000 FT AND 315 KTS, HAD EVENTUALLY 1.4 CABIN DIFFERENTIAL 5000 FT CABIN ALTITUDE. LT ENGINE BLEED PRESSURE 24Mar 26, 2018 · N791FD · Boeing 757222 · Pneumatic Distribution SystemSDR FDEA201803040587Flap Track · looseLOOSE NR 2 FLAP TRACK AFT ATTACH POINT, LEFT WING OUTBOARD FLAP. REMOVED THE FLAP TRACK ASSY, PERFORMED DVI INSPECTION OF THE FLAP TRACK AND ASSOCIATED COMPONENTS, REINSTALLED THE FLAP TRACK ASSY, AND PERFORMED A SATISFACTORY ADJUSTMENT AND TEST OF LEFT OUMar 4, 2018 · N791FD · Boeing 757222 · Trailing Edge FlapsSDR FDEA201803040586Flap Track · looseRT WING OB FLAP INBD TRACK IS LOOSE. REMOVED THE FLAP TRACK ASSY, PERFORMED DVI INSPECTION OF THE FLAP TRACK AND ASSOCIATED COMPONENTS, REINSTALLED THE TRACK ASSY, AND PERFORMED SATISFACTORY ADJUSTMENT AND TEST OF RIGHT OTBD FLAP ASSY IAW AMM 27-51-31-2, 27-Mar 4, 2018 · N791FD · Boeing 757222 · Trailing Edge FlapsSDR FDEA201803010546Skin · dentedC-1 DOOR, EXTERIOR SKIN HAS TWO DENTS AT BS 618, MID AREA OF DOOR. REPAIRED THE CARGO DOOR SKIN IAW SRM 52-30-01-2R, REP 4.Mar 1, 2018 · N791FD · Boeing 757222 · Cargo/Baggage DoorsSDR FDEA201802230477Skin · dentedRIGHT HORIZONTAL STAB LOWER SKIN DENTED. REPAIRED THE RT HORIZONTAL STAB LOWER SKIN IAW SRM 51-20-10-2R, 51-70-10-2R, REP 3 & 4, AND EA F-5510-T0324332 P3.Feb 23, 2018 · N791FD · Boeing 757222 · Horizontal Stabilizer, Plate/SkinSDR FDEA201702150568Pushrod · failedR1 DOOR FAILED DOOR EMERGENCY MECHANISM SYSTEM TEST. REPLACED R1 DOOR EMERG PWR TRIGGER MECH PUSH ROD AND ROD END REF AMM 52-11-32-4.Feb 15, 2017 · N791FD · Boeing 757222 · Service DoorsSDR FDEA201601220284Skin · dentedINCOMING, DENT IN FUSELAGE EXTERIOR SKIN, 18" FWD OF THE E & E BAY ENTRANCE WAY. ACCOMPLISHED EA F-5330-T0322892 PT 1. FUSELAGE PLATES & SKINS, FUSELAGE SKIN. REPAIR STATION 439 - 446, STRINGER 27L - 28L. THIS IS A CAT B REPAIR. REFERENCE FAA FORM 8100-9 Jan 22, 2016 · N791FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201601080090Stringer · dentedSTATION 430, STRINGER 18R, AFTER REMOVAL OF SKIN REPAIR, FOUND STRINGER DENTED. EVALUATED DENT IN STRINGER, FOUND NO ALLOWABLE DAMAGE FOR S/F ACFT. R & R STRINGER, STATION 395 - 439, STRINGER 18R IAW SRM 51-40-02. CAT A MAJOR REPAIR.Jan 8, 2016 · N791FD · Boeing 757222 · Fuselage Main, Longeron/StringerSDR FDEA201601060063Skin · gougedRIGHT WING INBD TOP FLAP, TOP SIDE HAS GOUGE & POSSIBLE CRACK IN SKIN. REPAIRED RT WING INBD TOP FLAP, TOP SKIN SURFACE IAW-SRM-51-70-07 CAT A MAJOR REPAIR, REF EA F-5750-T0322458 PT 1.Jan 6, 2016 · N791FD · Boeing 757222 · Trailing Edge FlapsSDR FDEA201601060062Skin · gougedRIGHT WING INBD TOP FLAP, TOP SIDE HAS GOUGE & POSSIBLE CRACK IN SKIN.Jan 6, 2016 · N791FD · Boeing 757222 · Trailing Edge FlapsSDR FDEA201512304107Skin · dentedINCOMING FUSELAGE SKIN DENT, BS 467, STRINGER 19R, DENT WAS FOUND OUT OF LIMITS DUE TO PROXIMITY TO THE LAP JOINT FASTENER LOCATIONS. ACCOMPLISHED EA F-5330-T0322263 PT 1 DATED DEC 15 2015. FUSELAGE PLATES & SKINS, DENT & GOUGE REWORKED. THIS IS A CAT B RDec 30, 2015 · N791FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201512244075Door Frame · crackedPASSENGER DOORS, CRACK NOTED ON NR 2R, PAX DOOR INNER CHORD OF THE DOOR FRAME AT THE UPPER HINGE CUT OUT. REPAIRED R2 DOOR FWD FRAME IAW SRM 52-10-02-2R REPAIR 1, REPAIR CLASSIFIED AS A CAT B MAJOR REPAIR. COMPLIED WITH EA F-5210-T0322556 PT 1 RELEASE DATE ODec 24, 2015 · N791FD · Boeing 757222 · Passenger/Crew DoorsSDR FDEA201512184027Longeron · dentedAFTER REMOVAL OF EXISTING SKIN REPAIR, STATION 1725, STRINGER 17L, FOUND DENT IN LONGERON. R & R LONGERON, LOWER CHORD IAW SRM-51-40-02. CAT A MAJOR REPAIR. FABRICATED ON T15 1171504 & DWG 145N9202-5.Dec 18, 2015 · N791FD · Boeing 757222 · Fuselage Main, Longeron/StringerSDR FDEA201512164019Skin Panel · corrodedPITTING CORROSION AT LAP SEAM, STRINGER 19R, BS 740 - 760. ACCOMPLISHED EA F5330-T0322184, PART 1 FUSELAGE PLATES & SKINS CORROSION REWORK. THIS IS A CAT B REPAIR. REF FORM 8110-3 DATED 12 08 2015. MAJOR REPAIR.Dec 16, 2015 · N791FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201512103969Skin · damagedMAIN DECK CARGO DOOR HAS PUNCTURE DAMAGE AT STRINGER 9, STATION 510 & A CREASE THAT EXTENDS FROM THE TOP OF THE PUNCTURE DAMAGE TO STRINGER 7. THERE IS ALSO A GOUGE JUST FWD OF THE PUNCTURE DAMAGE. REPAIRED MAIN DECK CARGO DOOR, BETWEEN STATION 500 & 520, BEDec 10, 2015 · N791FD · Boeing 757222 · Cargo/Baggage DoorsSDR FDEA201512083950Adapter · corrodedFUEL TANKS, LT WING TANK OVERWING FILL PORT ADAPTER MATING SURFACE CORRODED. REMOVED CORROSION FROM LT OVERWING FILL PORT ADAPTER MATING SURFACE IAW SRM 51-10-02, OUT OF LIMITS IAW SRM 57-20-01-1A STEP 3E. REPAIRED LT WING TANK FILL PORT ADAPTER MATING SURFADec 8, 2015 · N791FD · Boeing 757222 · Wing Miscellaneous StructureSDR FDEA201512083948Frame · corrodedAFT CARGO BAY FRAME, BS 1200 LBL 2.9 TO RBL 2.9, HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. REWORK AREA FOUND OUT OF LIMITS IAW SRM 53-00-07-1 FIG 101 DETAIL II. R & R FRAME IAW SRM 51-40-02 & DWG 146N1028 CAT A REPAIR. MAJOR REPAIR.Dec 8, 2015 · N791FD · Boeing 757222 · Fuselage Main, FrameSDR FDEA201512073938Adapter · corrodedFUEL TANKS, RT WING TANK OVERWING FILL PORT ADAPTER MATING SURFACE CORRODED. REMOVED CORROSION FROM RT OVERWING FILL PORT ADAPTER MATING SURFACE IAW SRM 51-0-02, OUT OF LIMITS IAW SRM 57-20-01-1A STEP 3E. REPAIRED RT WING OVERWING FILL PORT ADAPTER MATING SUDec 7, 2015 · N791FD · Boeing 757222 · Fuel StorageSDR FDEA201512073939Door Sill · corrodedAFT CARGO DOOR, LOWER SILL INBD CHORD, LOWER SURFACE UNDER & AROUND NUTPLATES, CORRODED. REMOVED CORROSION IAW SRM 51-10-02. NO ALLOWABLE DAMAGE NOTED IN SRM. R & R INBD UPPER CHORD FROM STATION 1360 - 1460, IAW SRM 51-40-02 & DWG 146N8522. MAJOR REPAIRDec 7, 2015 · N791FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201512033882Frame · corrodedAFT PIT FRAME STATION 1340, STRINGER 26R HAS CORROSION. REMOVED CORROSION IAW SRM-51-10-02, REWORK AREA, FOUND OUT OF LIMITS IAW SRM-53-00-07-1 FIG 101 DETAIL II. R & R FRAME AT STATION 1340 FROM STRINGER 24L - 24R IAW SRM-51-40-02 & DWG 146N1008 CAT A MAJORDec 3, 2015 · N791FD · Boeing 757222 · Fuselage Main, FrameSDR FDEA201512033881Skin · damagedINCOMING, LIGHTNING STRIKE BLEND OUT REPAIR THAT EXCEEDS THE SRM LIMITS AT BS 853, STRINGER 8L, 6TH & 7TH RIVETS FWD OF BS 860. REF UAL-IND-00-01028F. REPAIRED INCOMING BLENDED OUT AREA IAW-SRM-53-00-01 FIG 201 REPAIR 15 AT STATION 840- 860, BETWEEN STRINGEDec 3, 2015 · N791FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201511243773Seat Track · crackedSEAT TRACK STATION 780 - 879, RBL 45 IS CRACKED AT A F/P HOLE TO THE EDGE OF THE OTBD FLANGE. R & R SEAT TRACK IAW SRM-51-40-02, SRM-53-30-52-01 & DWG 143N5085, STATION 780 - 879, RBL 45, CAT A MAJOR REPAIR.Nov 24, 2015 · N791FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201511103551Skin · dentedPROTRUDING DENT BS 1543 IN FUSELAGE SKIN, 2.5" ABOVE STRINGER 27L. REPAIRED SKIN AT BS 1540, BETWEEN STRINGER 26L - 27L IAW-SRM-53-00-01 FIG 201 REPAIR 16. THIS IS CATEGORY B REPAIR, MAJOR.Nov 10, 2015 · N791FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201510293407Crease Beam · crackedRIGHT INNER CHORD AT STATION 1682 HAS A CRACK. WORK ACCOMPLISHED ON WC 60005228370001 & EA 757-5365-16-F5079 REV DECEMBER 16 2015. FUSELAGE FLOOR STRUCTURE, RT INBD CREASE BEAM REPAIR AT STATION 1681, WL 208.10, REFERENCE FORM 8110-3. THIS NON-ROUTINE IS FOOct 29, 2015 · N791FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201510293406Skin · damagedFUSELAGE SKIN STATION 1580, BETWEEN STRINGER 27L - 28L, HAS ELONGATED HOLES. REPAIRED SKIN IAW-SRM-53-00-01 FIG 201 REPAIR 15. THIS IS CATEGORY B REPAIR, MAJOR REPAIR.Oct 29, 2015 · N791FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201510283397Seat Track · misalignedINCOMING SEAT TRACK AT RBL 24, STATION 418 - 440, IS MISALIGNED. REMOVED SEAT TRACK IAW SRM 51-40-02. FABRICATED NEW SEAT TRACK IAW DWG 141N5131, PN FX 141N5131-40. INSTALLED NEW SEAT TRACK IAW DWG 141N5131. MAJOR REPAIR.Oct 28, 2015 · N791FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201510273382Floorbeam · corrodedCABIN FLOORBEAM AT STATION 1681, RBL 10.5 45.50, SEVERAL AREAS UNDERNEATH NUTPLATES HAS CORROSION. R & R THE FLOORBEAM IAW SRM 51-40-02 & IAW DWG NR 146N5091. CAT A MAJOR REPAIR. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101 DETAIL III. MAJOct 27, 2015 · N791FD · Boeing 757222 · Fuselage Main, Floor BeamSDR FDEA201510223312Door Frame · corrodedAFT CARGO DOOR SURROUND, BS 1400, RBL12, FWD SIDE OF FRAME CORRODED. REMOVED CORROSION IAW SRM 51-10-02. REWORKED AREA WAS FOUND OUT OF LIMITS IAW SRM 53-00-07-1 FIG 101 DETAIL II. R & R FRAME AT STATION 1400, FROM 24L - 27R IAW SRM 51-40-02 & DWG 146N1011.Oct 22, 2015 · N791FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201510153235Frame · gougedAFT CARGO COMPARTMENT AT BS 1540, BETWEEN STRINGER 26R & 27R, FRAME GOUGED. R & R FRAME IAW-SRM-51-40-02 & DWG 146N1030. CAT A MAJOR REPAIR.Oct 15, 2015 · N791FD · Boeing 757222 · Fuselage Main, FrameSDR FDEA201510153234Frame · corrodedBILGE AREA BS 1661, BETWEEN STRINGER 29L & 29R, FRAME HAS LIGHT SURFACE CORROSION. REMOVED CORROSION AT FRAME STATION 1661, BETWEEN STRINGER 24R & 24L IAW SRM-51-10-02. ORIGINAL MAT .063, AFTER RE-WORK MATERIAL .052, A MATERIAL LOSS OF .011, WAS OUT OF LIMIOct 15, 2015 · N791FD · Boeing 757222 · Fuselage Main, FrameSDR FDEA201510153233Frame · corrodedAFT CARGO COMPARTMENT AT BS 1460, BETWEEN STRINGER 25L & 26L FRAME CORRODED. REMOVED CORROSION IAW SRM 51-10-02 AND FOUND TO BE OUT OF LIMITS IAW SRM-53-00-07-1A FIG 101 DET II. R & R FRAME IAW SRM-51-40-02 & DWG 146N1014. CAT A MAJOR REPAIR.Oct 15, 2015 · N791FD · Boeing 757200 · Fuselage Main, FrameSDR FDEA201509222911Switch · inoperativeFLIGHT 270, APPROX TWO HOURS AFTER TAKEOFF, EICAS MSG L, ENG BLEED VAL WITH CORRESPONDING L ENG BLEED OFF LIGHT ON P11 PANEL. SINCE THE RT ENG BLEED AIR WAS INOPERATIVE DUE TO A PRIOR MALFUNCTION, NO BLEED SOURCES WERE AVAILABLE TO OPERATE ENG ANTI-ICE, WING Sep 22, 2015 · N791FD · Boeing 757222 · Pneumatic Distribution System
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