# Service difficulty reports: N796FD

A list on [N796FD](https://openairdocs.org/aircraft/N796FD.md).

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

Page 1 of 2 · 60 reports

- [SDR FDEA202203110773](https://openairdocs.org/sdr/FDEA202203110773.md): None · none · Mar 11, 2022 · N796FD · Boeing 757200 · Emergency Lighting
  > L1 DOOR EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED INOP L1 DOOR EMERGENCY LIGHT. ALL WORK REFERENCED TO 757 AMM 33-51-06-2-1. OP'S CHECK GOOD.
- [SDR FDEA202104220980](https://openairdocs.org/sdr/FDEA202104220980.md): Cusp Web · cracked · Apr 22, 2021 · N796FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > MAIN CUSP AREA STA 640-660 LBL 62.5 AS VIEWED FROM BOTTOM FILLER PN BACF3F020B197NN CRACKED AT FASTENER LOCATION ACCOMPLISHED FEDEX EA # F-5321-T0361228-P1 FUSELAGE - CARGO COMP FLOORS - MAIN CABIN - STA 640 - LBL - 62.5 - CRACKED
- [SDR FDEA202104220973](https://openairdocs.org/sdr/FDEA202104220973.md): Seat Track · cracked · Apr 22, 2021 · N796FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN - STA 580 SEAT TRACK IS CRACKED ACCOMPLISHED FEDEX EA # F-5310-T0361001-P1: FUSELAGE - MAINFRAME - SEAT TRACK STA 580 LBL 45, CRACKED FLANGE
- [SDR FDEA202104200958](https://openairdocs.org/sdr/FDEA202104200958.md): Stub Frame · cracked · Apr 20, 2021 · N796FD · Boeing 757222 · Fuselage Main, Structure
  > MAIN CABIN FLOOR - STUB BEAM IS CRACKED REPAIRED STUB BEAM IAW FEDEX DWG SR57-53-004 AND EA: F-5310-T0361029: FUSELAGE - MAINFRAME - STA 580 FLOOR BEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR - REPAIR DOCUMENTATION AND REPETITIVE INSPECTIONS PER SR57
- [SDR FDEA2020090952126](https://openairdocs.org/sdr/FDEA2020090952126.md): Nozzle · cracked · Sep 5, 2020 · N796FD · Boeing 757222 · Engine Collector/Tailpipe/Nozzle
  > NR 2 ENGINE EXHAUST NOZZLE 9 O'CLOCK POSITION MOUNT FLANGE CRACKED. REPAIRED NR 2 ENGINE EXHAUST NOZZLE 9 O'CLOCK POSITION MOUNT FLANGE, PER CMM 78-11-01 REP 2-1.
- [SDR FDEA202008312072](https://openairdocs.org/sdr/FDEA202008312072.md): Transition Panel · gouged · Aug 31, 2020 · N796FD · Boeing 757236 · Fuselage Miscellaneous Structure
  > AFT CARGO PIT LH STA 1510 TRANSITION PANEL HAS GOUGE REPAIRED TRANSITION PANEL L/H STA 1510 IAW B757 SRM 53-00-53-2R DUE TO TRANSITION PANEL GOUGE FOUND TO BE OUT OF LIMITS PER B757 SRM 53-00-53-1A, DETAIL V.
- [SDR FDEA202009092066](https://openairdocs.org/sdr/FDEA202009092066.md): Fairing · cracked · Aug 29, 2020 · N796FD · Boeing 757222 · Horizontal Stabilizer Structure
  > TAIL SECTION LT LOWER HORIZONTAL STAB SEAL FAIRING DENTED/CRACKED. REPAIRED TAIL SECTION LT LOWER HORIZONTAL STAB SEAL FAIRING, IAW FEDEX EA NR F-5350- T0356088-P1 FUSELAGE-AERODYNAMIC FAIRINGS-LT HORIZONTAL STABILIZER TO BODY LWR BLADE ASSY DAM.
- [SDR FDEA2020083192066](https://openairdocs.org/sdr/FDEA2020083192066.md): Fairing · cracked · Aug 29, 2020 · N796FD · Boeing 757222 · Horizontal Stabilizer Structure
  > TAIL SECTION L/H LOWER HORIZONTAL STAB. SEAL FAIRING DENTED/ CRACKED. REPAIRED TAIL SECTION L/H LOWER HORIZONTAL STAB SEAL FAIRING IAW FEDEX EA# F-5350- T0356088
- [SDR FDEA202008272044](https://openairdocs.org/sdr/FDEA202008272044.md): Angle · cracked · Aug 27, 2020 · N796FD · Boeing 757222 · Nacelle/Pylon Miscellaneous Structure
  > NR 2 PYLON 445BL HAS A CRACKED CLIP. REMOVED, FABBED, AND REPLACED NEW CLIP IAW BOEING DWG 313N5022 REV AB.
- [SDR FDEA202008272043](https://openairdocs.org/sdr/FDEA202008272043.md): Barrier · cracked · Aug 27, 2020 · N796FD · Boeing 757222 · Nacelle/Pylon Miscellaneous Structure
  > NR 2 ENGINE INBOARD UPPER PYLON FWD AREA JUST ABOVE THE INBOARD T/R PLASTIC SHIELD IS CRACKED IN TWO PLACES. REPAIRED NR 2 ENGINE INBOARD AFT FLUID BARRIER ON 2 EA AREAS, IAW FEDEX EA F-5450-T0356144-P1, NACELLES/PYLON - WING PYLON/STRUT NR #2 (RT) PYLON INBO
- [SDR FDEA202008262035](https://openairdocs.org/sdr/FDEA202008262035.md): Bracket · cracked · Aug 26, 2020 · N796FD · Boeing 757222 · Wing Miscellaneous Structure
  > RT WING FUEL DOOR SWITCH BRACKET CRACKED STREAMER ATTACHED. REMOVED AND REPLACED BRACKET PER BOEING DWG NR 284N1138 AND B757 SRM 51-40-02.
- [SDR FDEA202008252021](https://openairdocs.org/sdr/FDEA202008252021.md): Floorbeam · corroded · Aug 25, 2020 · N796FD · Boeing 757222 · Fuselage Main, Floor Beam
  > CABIN FLOOR BEAM CORRODED BS 375, BL354L. REMOVED CORROSION IAW B757 SRM 51-10-02. DAMAGE FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-51-1A. ACCOMPLISHED FLOOR BEAM REPAIR IAW FEDEX EA "F-5310-T0356115-P1. FUSELAGE-MAINFRAME, MAIN CABIN FLOOR BEAM STA 377
- [SDR FDEA202008252019](https://openairdocs.org/sdr/FDEA202008252019.md): Seat Track · corroded · Aug 25, 2020 · N796FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK CORRODED BS 342- BS 372, BL 7L REMOVED CORROSION AS REQUIRED IAW B757 SRM 51-10-02. MAX ALLOWABLE MAT REMOVAL.020, REMOVED.030. FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-52-1A FIG 101 DET "I". FABRICATED NEW SEAT TRACK AND INSTALLED I
- [SDR FDEA202008252020](https://openairdocs.org/sdr/FDEA202008252020.md): Seat Track · corroded · Aug 25, 2020 · N796FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK CORRODED BS 365, BL 44R - BL 47R. ACCOMPLISHED EA# F-5310-T0356090-P1 FUSELAGE - MAINFRAME - SEAT TRACK - STA 365 - RBL 45.50 - CORROSION.
- [SDR FDEA2020082621983](https://openairdocs.org/sdr/FDEA2020082621983.md): Floorbeam · corroded · Aug 22, 2020 · N796FD · Boeing 757222 · Fuselage Main, Floor Beam
  > FLOOR BEAM NUTPLATE IS CORRODED BS 1681-RBL47. REMOVED NUTPLATE BRACKET IAW B757 SRM 51-40-02. MAT ID 7075-T6 ALUMINIUM SHEET PO NR 964704.1, IAW BOEING PL 146N5693 REV C AND BOEING DWG 146N5693 REV B. FABRICATED NUTPLATE STRIP IAW BOEING DWG 146N5693 REV B.
- [SDR FDEA202008201947](https://openairdocs.org/sdr/FDEA202008201947.md): Seal · cracked · Aug 20, 2020 · N796FD · Boeing 757222 · Engine Collector/Tailpipe/Nozzle
  > #1 ENG EXHAUST NOZZLE O/B UPPER SPRING LEAF CRACKED REMOVED AND REPLACED SPRING LEAF PER B757 SRM 51-40-02-0G AND REF IPC 78-11-01-03
- [SDR FDEA2020082091939](https://openairdocs.org/sdr/FDEA2020082091939.md): Bulkhead · cracked · Aug 19, 2020 · N796FD · Boeing 757222 · Nacelle/Pylon, Bulkhead/Firewall
  > #2 PYLON HYDRAULIC BAY,AFT OF BULKHEAD THE OTBD LWR FWD CORNER ATTACH CLIP IS CRACKED REMOVED AND REPLACED CLIP PER BOEING DWG #313N3052
- [SDR FDEA201903130623](https://openairdocs.org/sdr/FDEA201903130623.md): Wire · broken · Mar 13, 2019 · N796FD · Boeing 757222 · Light System Wiring
  > FOUND EMERGENCY EXIT LIGHT AFT OF THE COCKPIT DOOR INOP REMOVED THE LIGHT FOUND 2 BROKEN WIRES REPINNED CONNECTOR D4524 ON THE EMERGENCY EXIT LOCATION LIGHT. LIGHT OPS CHECKS NORMAL REF SWP 33-51-12 PG 904 NO PART WAS CHANGED.
- [SDR FDEA201803130654](https://openairdocs.org/sdr/FDEA201803130654.md): Light · inoperative · Mar 13, 2018 · N796FD · Boeing 757222 · Emergency Lighting
  > DURING A SERVICE CHECK, FOUND THE EXTERNAL RT DOOR SLIDE LIGHT INOPERATIVE. REPLACED THE LAMP, OPS CHECKED GOOD IAW 33-51-06-2-1.
- [SDR FDEA201803070625](https://openairdocs.org/sdr/FDEA201803070625.md): Wire Harness · damaged · Mar 7, 2018 · N796FD · Boeing 757222 · Air Conditioning System Wiring
  > EQUIPMENT OVERHEAT EICAS MESSAGE DURING CLIMBOUT. HAD A STATUS MESSAGE FOR EQPT CLG FLOW AND EQPT CLG FAN, CIRCUIT BREAKER TRIPPED FOR ALTERNATE COOLING FAN. AFTER TOUBLESHOOTING, FOUND WIRE BUNDLE W4104, CONTAINING WIRES W4104-0008-16, -0009-16, -0010-16
- [SDR FDEA201711123236](https://openairdocs.org/sdr/FDEA201711123236.md): Skin · punctured · Nov 12, 2017 · N796FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > PRIOR TO LOADING, RAMP DISCOVERED PUNCTURE IN FUSELAGE FWD OF MAIN CARGO DOOR. REPAIRED IAW EA F-5330-T0336569 PT 1 AND 2.
- [SDR FDEA201710243033](https://openairdocs.org/sdr/FDEA201710243033.md): Lamp · inoperative · Oct 24, 2017 · N796FD · Boeing 757222 · Emergency Lighting
  > R1 EMERGENCY SLIDE LIGHT INOPERATIVE DURING A TEST. REPLACED THE LAMP AND OPS CHECKED NORMAL IAW MM 33-51-06. ACFT OK FOR SERVICE.
- [SDR FDEA201608152891](https://openairdocs.org/sdr/FDEA201608152891.md): Shear Tie · corroded · Aug 15, 2016 · N796FD · Boeing 757222 · Fuselage Internal Mounting Structure
  > AFT FUSELAGE SKIN HAS A BULGED AREA BS 1540 STRINGER 28R. FOUND SHEAR TIE CORRODED. REMOVED IAW SRM 51-40-02-OG, FABRICATED IAW B DWG 140N2002, REV B, HEAT TREATED IAW FORM FAS 0119, REV O AND INSTALLED SHEAR TIE IAW DWG 140N2002, REV B AND SRM 51-40-02-OG
- [SDR FDEA201503180959](https://openairdocs.org/sdr/FDEA201503180959.md): Cable · unsecure · Mar 18, 2015 · N796FD · Boeing 757222 · Emergency Equipment
  > R1 DOOR DISARMING HANDLE WILL ONLY GO HALFWAY, WILL NOT MOVE INTO THE GREEN ZONE ENTIRELY. IAW AMM 25-66-10-2-0 FOUND CORD FROM SLIDE STUCK IN FWD GIRT BAR. SECURED CORD, GIRT BAR & SLIDE CHECKED NORMAL.
- [SDR FDEA201411263899](https://openairdocs.org/sdr/FDEA201411263899.md): Sliding Window · out of adjust · Nov 26, 2014 · N796FD · Boeing 757222 · Flight Compartment Windows
  > CAPTAIN'S SLIDING WINDOW WILL NOT OPEN. ADJUSTED CAPTAIN`S SLIDING WINDOW IAW AMM 56-11-02-5. OPERATIONS CHECKED GOOD.
- [SDR FDEA201409042452](https://openairdocs.org/sdr/FDEA201409042452.md): Repair · scratched · Sep 4, 2014 · N796FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN, EXISTING REPAIR FINDING LT SIDE THERE ARE SCRATCHES ON THE EXTERIOR OF THE EXISTING REPAIR BODY STATION 439 - 449 BETWEEN STRINGER 26 - 27. REMOVED & NEW REPAIR CARRIED OUT AS PER PART 1 OF EA F-5310 -T0310235. TITLE FUSELAGE MAIN FRA
- [SDR FDEA201408272322](https://openairdocs.org/sdr/FDEA201408272322.md): Frame · damaged · Aug 27, 2014 · N796FD · Boeing 757222 · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT LT SIDE EXISTING REPAIR FINDING BS 1580 AT STRINGER 25 - 26. AFTER OUTER J CHANNEL REMOVED FOUND ELONGATED HOLE. AFT CARGO COMPARTMENT AT STA 1580 STR 25-26 ELONGATED HOLE ACCOMPLISH AS PER EA 5310- T0310064 P1 TITLE: FUSELAGE - MAINFR
- [SDR FDEA201408182196](https://openairdocs.org/sdr/FDEA201408182196.md): Fastener · corroded · Aug 18, 2014 · N796FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE AFT CARGO EXISTING REPAIR RT SIDE THE FASTENERS ARE CORRODED AT BS 1420 - 1440 & STRINGER 26 - 27. ACCOMPLISHED F-5330-T0310527 PT 1 TITLE: AD 2006-11-11- FUSELAGE SKIN REPAIR NR 2 CARGO DOORWAY LOWER AFT EDGE BETWEEN BS 1410 TO BS 1445. REPAIR CLA
- [SDR FDEA201408182198](https://openairdocs.org/sdr/FDEA201408182198.md): Fastener · corroded · Aug 18, 2014 · N796FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE AFT CARGO EXISTING REPAIR RT SIDE THE FASTENERS ARE CORRODED AT BS 1440 - 1460 & STRINGER 26 - 27. ACCOMPLISHED EA F-5330-T0310527 P1 TITLE AD 2006-11-11 FUSELAGE SKIN REPAIR NR 2 CARGO DOORWAY LOWER AFT EDGE BETWEEN BS 1410 TO BS 1445. REPAIR CLASS
- [SDR FDEA201408182197](https://openairdocs.org/sdr/FDEA201408182197.md): Fastener · corroded · Aug 18, 2014 · N796FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE AFT CARGO EXISTING REPAIR RT SIDE THE FASTENERS ARE CORRODED AT BS 1440 - 1460 & STRINGER 25 - 26. ACCOMPLISHED EA F-5330-T0310527 P1 TITLE: AD 2006-11-11 FUSELAGE SKIN REPAIR NO.2 CARGO DOORWAY LOWER AFT EDGE BETWEEN BS 1410 TO BS 1445. REPAIR C
- [SDR FDEA201408122146](https://openairdocs.org/sdr/FDEA201408122146.md): Fitting · chafed · Aug 12, 2014 · N796FD · Boeing 757222 · Nacelle/Pylon, Bulkhead/Firewall
  > NUMBER 2 PYLON AFT BULKHEAD OTBD LOWER CORNER ANGLE FOUND CHAFED MARK. REPAIR CARRIED OUT AS PER EA F-5450-T0311030A PART 1 [REPAIR ON NR 2 PYLON AFT BULKHEAD FITTING, OUTBD FLANGE LOWER CORNER ]. REPAIR IS MAJOR.
- [SDR FDEA201408122145](https://openairdocs.org/sdr/FDEA201408122145.md): Fitting · chafed · Aug 12, 2014 · N796FD · Boeing 757222 · Nacelle/Pylon, Bulkhead/Firewall
  > NR 1 PYLON AFT BULKHEAD OTBD LOWER CORNER ANGLE CHAFED. REPAIR CARRIED OUT AS PER EA F-5450-T0311029A PART 1 [REPAIR ON NR 1 PYLON AFT BULKHEAD FITTING, OUTBD FLANGE LOWER CORNER]. REPAIR IS MAJOR.
- [SDR FDEA201407302011](https://openairdocs.org/sdr/FDEA201407302011.md): Frame · cracked · Jul 30, 2014 · N796FD · Boeing 757222 · Fuselage Main, Frame
  > BS 1681 STRINGER 7L FRAME INBD FLANGE AFT EDGE FOUND CRACKED. REPAIRED IAW EA F-5310-T0309884. CLASSIFIED AS MINOR.
- [SDR FDEA201407302004](https://openairdocs.org/sdr/FDEA201407302004.md): Skin · damaged · Jul 30, 2014 · N796FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN HAD A LIGHTNING STRIKE AT BS 1400 - 1420 BETWEEN STRINGER 27 - 28L. REPAIRED IAW EA F-5310-T0310066 PART 1. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201407292001](https://openairdocs.org/sdr/FDEA201407292001.md): Stringer · cracked · Jul 29, 2014 · N796FD · Boeing 757222 · Fuselage Main, Longeron/Stringer
  > BS 1500, STRINGER 14R CRACKED. REPAIRED IAW EA F-5310-T0309688 PART 1. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201407292000](https://openairdocs.org/sdr/FDEA201407292000.md): Floorbeam · corroded · Jul 29, 2014 · N796FD · Boeing 757222 · Fuselage Main, Floor Beam
  > CABIN FLOORBEAM CORRODED ON THE UPPER SIDE AT BS 365 FROM RBL 10 TO THE RT SIDE. REPAIRED IAW E.A F-5310- T0310519 B PART 1. PEPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201407251962](https://openairdocs.org/sdr/FDEA201407251962.md): Skin · chafed · Jul 25, 2014 · N796FD · Boeing 757222 · Trailing Edge Flaps
  > RIGHT WING OTBD TE MAIN FLAP NOSE SKIN LE FOUND CHAFED AT 2.5 INCHES FROM OTBD EDGE. REPAIRED IAW EA F-5750-T0309844 P1. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201407171833](https://openairdocs.org/sdr/FDEA201407171833.md): Stringer · cracked · Jul 17, 2014 · N796FD · Boeing 757222 · Fuselage Main, Longeron/Stringer
  > CABIN STATION 1521 - 1519 STRINGER 14R, STRINGER CRACKED. COMPLIED WITH EA F-5310-T0309688 PART 1 TITLE FUSELAGE MAINFRAME SPLICE REPAIR FOR CRACKED STRINGER. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201407171834](https://openairdocs.org/sdr/FDEA201407171834.md): Stringer · corroded · Jul 17, 2014 · N796FD · Boeing 757222 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT STATION 1618 STRINGER 18L, STRINGER HAS CORROSION FOUND AFTER SPLICE. REMOVED IAW SNRM N02602. ACCOMPLISHED EA F-5310-T0309662, TITLE FUSELAGE MAINFRAME SPLICE REPAIR FOR CORRODED STRINGER 18L AT STATION 1618. REPAIR CLASSIFIED AS MAJO
- [SDR FDEA201407071648](https://openairdocs.org/sdr/FDEA201407071648.md): Splice Plate · gouged · Jul 7, 2014 · N796FD · Boeing 757222 · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT, STATION 1520, STRINGER 23R - 25R FRAME SPLICE PLATE HAS GOUGE MARKS. GOUGED SPLICE PLATE AT STA 1520, STR 23R-25R, REMOVED AND REPLACED WITH NEW SPLICE PLATE FABRICATED AS PER DWG 146N1042 SHT 4 REV B AND INSTALLED IAW DWG 146N1017 SHT
- [SDR FDEA201407071647](https://openairdocs.org/sdr/FDEA201407071647.md): Stringer Splice · corroded · Jul 7, 2014 · N796FD · Boeing 757222 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT STATION 1618 STRINGER 20L, STRINGER SPLICE CORROSION AFTER ACCESS. REPAIR CARRIED OUT IAW EA F-5310-T0310628 PART 1. LOCAL FABRICATION TO REPLACE CORRODED THROUGH STRINGER CHANNEL SPLICE. REPAIR IS MAJOR.
- [SDR FDEA201407041622](https://openairdocs.org/sdr/FDEA201407041622.md): Skin · scratched · Jul 4, 2014 · N796FD · Boeing 757222 · Passenger/Crew Doors
  > CABIN L2 DOOR OUTER SKIN FOUND SCRATCHES. COMPLIED WITH EA F-5210-T0310189. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201407021609](https://openairdocs.org/sdr/FDEA201407021609.md): Strap · corroded · Jul 2, 2014 · N796FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > EMPENNAGE APU AIR INLET DOOR CUT OUT MIDDLE STRAP FOUND CORROSION AT STATION 1825 STRINGER 3R - 6R AFTER APU AIR INLET DOOR HOUSING REMOVED. CORROSION REMOVED FOUND OUT OF LIMIT AS PER SRM 53-80-15 TABLE 101 ALLOWABLE DAMAGE 1 REV 112 & REPAIR CARRIED OUT AS
- [SDR FDEA201407021607](https://openairdocs.org/sdr/FDEA201407021607.md): Seat Track · corroded · Jul 2, 2014 · N796FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN STATION 688 - 710 RBL 24.75 SEAT TRACK BOTTOM FOUND CORROSION. CORROSION REMOVED AS PER SRM 51-10-02 REV 112. REWORKED AREA CLEANED UP DEPTH OF 0.065" FOUND EXCEED 0.040" LIMIT AS PER SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 REV 112. SEAT TRACK REPAIR
- [SDR FDEA201407021605](https://openairdocs.org/sdr/FDEA201407021605.md): Rib · worn · Jul 2, 2014 · N796FD · Boeing 757222 · Trailing Edge Flaps
  > LEFT WING INBD TE AFT FLAP INBD RIB FOUND WORN AT AFT FLAP STATION 78.30, IAW SRM 57-53-02 IDENTIFICATION 1 FIG 1 SHEET 4 OF 8. RIB REMOVED AND REPLACED WITH NEW RIB IAW DWG 113N2800 SHT 4 REV B AND SRM 51-40-02 REV 112. REPAIR IS MAJOR.
- [SDR FDEA201406281572](https://openairdocs.org/sdr/FDEA201406281572.md): Fitting · damaged · Jun 28, 2014 · N796FD · Boeing 757222 · Nacelle/Pylon, Attach Fittings
  > DURING COMPLYING EO F-7120-7-5000 PT1, FIG 1 SHEET 1 STEP 7, AFTER REMOVAL OF NR 1 PYLON AFT ENG MOUNT FWD & AFT SHEAR BOLT FLANGE BUSHINGS, FOUND BUSHING HOLES TWO EACH OUT OF DWG TOLERANCE. REPAIR CARRIED OUT AS PER EA F-5450-T0309191 PART 1 [ PYLONS STRUCT
- [SDR FDEA201406281571](https://openairdocs.org/sdr/FDEA201406281571.md): Fitting · damaged · Jun 28, 2014 · N796FD · Boeing 757222 · Nacelle/Pylon, Attach Fittings
  > DURING COMPLYING EO F-7120-7-5000 PT 1, FIG 1 SHEET 1 STEP 7, AFTER REMOVAL OF NR 2 PYLON AFT ENG MOUNT FWD & AFT SHEAR BOLT FLANGE BUSHINGS, HOLES TWO EACH OUT OF DWG TOLERANCE. REPAIR CARRIED OUT AS PER EA F-5450-T0309191 PART 1 [ PYLONS STRUCTURES - SB-757
- [SDR FDEA201406241534](https://openairdocs.org/sdr/FDEA201406241534.md): Strap · corroded · Jun 24, 2014 · N796FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > EMPENNAGE APU AIR INLET DOOR CUT OUT FWD STRAP HAS CORROSION AT STATION 1787 STRINGER 3R - 6R AFTER APU AIR INLET DOOR HOUSING REMOVED. STA 1787 STR 3R - 6R APU INLET DOOR CUT-OUT CORROSION THROUGH FWD STRAP REMOVED AND REPLACED WITH NEW STRAP P/N 148N3138-
- [SDR FDEA201406211500](https://openairdocs.org/sdr/FDEA201406211500.md): Stringer Splice · corroded · Jun 21, 2014 · N796FD · Boeing 757222 · Fuselage Main, Longeron/Stringer
  > AFT CARGO BAY BS 1617 STRINGER 18L, STRINGER SPLICE CORRODED. REMOVED AND REPLACED WITH NEW STRINGER SPLICE IAW DWG 146N3700 SHT.13 REV.B. MAJOR REPAIR.
- [SDR FDEA201406211504](https://openairdocs.org/sdr/FDEA201406211504.md): Seat Track · chafed · Jun 21, 2014 · N796FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > BS 860 - 880 LBL 24.75 SEAT TRACK INNER FLANGE FOUND CHAFED. CHAFE REMOVED IAW SRM 51-10-02 REV 112. FOUND OUT OF LIMITS IAW SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101 REV 112. REPAIRED IAW SRM 53-00-52 OPTION 1 REPAIR 1 FIG 201 REV 112. REPAIR CLASSIFIED AS

Next page: https://openairdocs.org/aircraft/N796FD/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'N796FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N796FD/reports

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