# Service difficulty reports: N777FD

A list on [N777FD](https://openairdocs.org/aircraft/N777FD.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 · 69 reports

- [SDR FDEA201905211105](https://openairdocs.org/sdr/FDEA201905211105.md): Girt Bar · defective · May 21, 2019 · N777FD · Boeing 757222 · Emergency Equipment
  > L1 SLIDE ARM LIGHT DOES NOT ILLUMINATE WHEN DOOR IS ARMED. REMOVED AND REPLACED L1 DOOR GIRT BAR P/N ON 140N2762-17 S/N FX0009 P/N OFF 140N2762-18 S/N LIA 7402 REF. AMM 52-11-25-5-0, A/C IS OK FOR SERVICE.
- [SDR FDEA2018111973267](https://openairdocs.org/sdr/FDEA2018111973267.md): Diaphragm · unknown · Nov 17, 2018 · N777FD · Boeing 757222 · Escape Slide
  > L1 SLIDE PACK FELL OUT OF DOOR RECESS WHEN DOOR OPENED FROM OUTSIDE. (DOOR NOT DISARMED FROM PREVIOUS FLIGHT). REPLACED DIAPHRAGM IN L1 DOOR EMERGENCY POWER RESERVOIR PER M.M. 12-15-10-3 & SERVICE SAME TO GRE
- [SDR FDEA201802080320](https://openairdocs.org/sdr/FDEA201802080320.md): Not Reported · unknown · Feb 8, 2018 · N777FD · Boeing 757222 · Hydraulic System, Main
  > LOST LEFT HYDRAULIC QUANITY & PRESSURE ON 5 MILE FINAL. RAN QRH AND LANDED. REMOVED AND REPLACED THE TEMP LINE IAW AMM 20-10-10-4-0. TESTED THE LT DOWNLOCK ACTUATOR AND LINES IAW AMM 32-32-02-4, NO LEAKS NOTED. RAN ENGINES IAW MM-3614 AND ACTUATED ALL FLI
- [SDR FDEA201711033140](https://openairdocs.org/sdr/FDEA201711033140.md): Wire · damaged · Nov 3, 2017 · N777FD · Boeing 757222 · Equipment/Furnishings Wiring
  > R1 SLIDE LIGHT INTERMITTENT, FOUND WIRE W3682-0003-20 AND WIRE W3682-0012-20 BROKEN APPROX 60 INCHES FROM SPLICE SP1478 AND SPLICE SP68. REPAIRED REF WDM 25-66-11 PG 901 AND SWPM. CKS OK. MEL CLEARED AND PLACARD REMOVED.
- [SDR FDEA201608052824](https://openairdocs.org/sdr/FDEA201608052824.md): Pitot Tube · damaged · Aug 5, 2016 · N777FD · Boeing 757222 · Pitot/Static System
  > BIRDSTRIKE ON DEPARTURE. LOST ALL AIRSPEED INDICATIONS AND ASSOCIATED ITEMS ON F/O'S SIDE. R & R F/O'S PITOT TUBE REF 34-11-01-4, THROUGH STEP 29, STEP 30, LEAKAGE TEST NEEDS ACCOMPLISHED. PERFORMED PITOT LEAK CHECK OF F/O'S PITOT TUBE IAW AMM 34-11-01-5.
- [SDR FDEA201603271093](https://openairdocs.org/sdr/FDEA201603271093.md): Collar · inoperative · Mar 27, 2016 · N777FD · Boeing 757222 · Passenger/Crew Doors
  > L1 DOOR HOLD OPEN LOCK INOPERATIVE. DOOR OPENS & SHUTS NORMALLY. R & R L1 DOOR HOLD OPEN LOCK COLLAR & CATCH IAW MM 52-11-08-8. OPERATIONS CHECKED GOOD.
- [SDR FDEA201602050459](https://openairdocs.org/sdr/FDEA201602050459.md): Stop Fitting · galled · Feb 5, 2016 · N777FD · Boeing 757222 · Passenger/Crew Doors
  > CABIN L1 DOOR, FWD EDGE NR 1 - 7 STOP PINS FOUND METAL GALLING. R & R IAW AMM 52-11-00 REV 114. ADJUSTMENT CHECK CARRIED OUT IAW AMM 52-11-00 REV 114. FOUND GOOD. REPAIR CLASSIFIED AS MINOR.
- [SDR FDEA201602050458](https://openairdocs.org/sdr/FDEA201602050458.md): Bearing · loose · Feb 5, 2016 · N777FD · Boeing 757222 · Passenger/Crew Doors
  > CABIN L1 DOOR, FWD EDGE LOWER LATCH CRANK FOUND LOOSEN AT SUPPORT BEARING AREA. L1 DOOR, FWD LOWER LATCH CRANK R & R IAW CMM 52-11-07 REV 114. L1 DOOR FWD LOWER LATCH CRANK SUPPORT BEARING R & R IAW SOPM 20-50-03 REV 127. ADJUSTMENT CHECK CARRIED OUT IAW AM
- [SDR FDEA201512294100](https://openairdocs.org/sdr/FDEA201512294100.md): Seat Track · damaged · Dec 29, 2015 · N777FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > BS 608, RBL 45.5, SEAT TRACK INNER FLANGE, FOUND ONE ELONGATED HOLE. REPAIRED IAW EA F-5310-T0321333. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201512284088](https://openairdocs.org/sdr/FDEA201512284088.md): Support Angle · corroded · Dec 28, 2015 · N777FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > BS 1681, R4 DOOR SCUFF PLATE SUPPORT ANGLE FOUND CORRODED. REPAIRED IAW EA F-5310-T0321518 PART 1. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201512133981](https://openairdocs.org/sdr/FDEA201512133981.md): Seat Track · damaged · Dec 13, 2015 · N777FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > BS 988, BL 45.5, SEAT TRACK CROWN, SUPPORT INNER FLANGE FOUND ONE ELONGATED HOLE. REPAIRED IAW EA F-5310-T0321399 PART 1. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201512103964](https://openairdocs.org/sdr/FDEA201512103964.md): Floorbeam · corroded · Dec 10, 2015 · N777FD · Boeing 757222 · Fuselage Main, Floor Beam
  > CABIN BS 1640, FLOORBEAM EXISTING REPAIR HAS CORROSION. COMPLIED WITH EA F-5310-T0321037 PART 1. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201512103963](https://openairdocs.org/sdr/FDEA201512103963.md): Floorbeam · corroded · Dec 10, 2015 · N777FD · Boeing 757222 · Fuselage Main, Floor Beam
  > BS 1640, FLOORBEAM HAS CORROSION. REPAIRED IAW EA F-5310-T0321037 PART 1. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201511293814](https://openairdocs.org/sdr/FDEA201511293814.md): Skin Panel · chafed · Nov 29, 2015 · N777FD · Boeing 757222 · Wing, Plate/Skin
  > RIGHT WING, OTBD NOSE SKIN FOUND CHAFED AT 2.5" FROM OTBD EDGE. NOSE SKIN R & R IAW SRM 51-40-02 REV 116 & DWG 113N3500 SHT 3 REV D. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201511253775](https://openairdocs.org/sdr/FDEA201511253775.md): Beam · gouged · Nov 25, 2015 · N777FD · Boeing 757222 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR LOWER EDGE BEAM HAS GOUGE MARKS. R & R WITH NEW LOWER EDGE BEAM IAW DWG NR 143N6603 SHT 9 REV F. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201511183690](https://openairdocs.org/sdr/FDEA201511183690.md): Support Beam · worn · Nov 18, 2015 · N777FD · Boeing 757222 · Nacelle/Pylon Miscellaneous Structure
  > NUMBER 2 PYLON, FAN COWL SUPPORT BEAM AFT WEB, OTBD DOUBLER AT NAC STATION 102.1, FOUND WEAR MARK.
- [SDR FDEA201511173656](https://openairdocs.org/sdr/FDEA201511173656.md): Doubler · debonded · Nov 17, 2015 · N777FD · Boeing 757222 · Trailing Edge Flaps
  > EXISTING REPAIR, WINGS RT SIDE, THERE IS A RT INBD FLAP LOWER SURFACE INBD PANEL REPAIR. THIS REPAIR REQUIRES EVALUATION IAW EO F-5100-7-5001 A4 PT 1, ATTACHMENT B, NO HISTORY. EXISTING REPAIR WAS EVALUATED IAW ATTACHMENT B OF EO F-5100-7-5001 A4 PART 1. FO
- [SDR FDEA201511173657](https://openairdocs.org/sdr/FDEA201511173657.md): Doubler · debonded · Nov 17, 2015 · N777FD · Boeing 757222 · Trailing Edge Flaps
  > EXISTING REPAIR, RT SIDE UPPER SIDE OF INBD MAIN FLAP PANEL. THIS REPAIR REQUIRES EVALUATION IAW EO F-5100-7-5001 A4 PT 1, ATTACHMENT B, NO HISTORY. EXISTING REPAIR WAS EVALUATED IAW ATTACHMENT B OF EO F-5100-7-5001 A4 PART 1. FOUND REPAIR DOUBLER DIS BONED
- [SDR FDEA201511173659](https://openairdocs.org/sdr/FDEA201511173659.md): Frame · damaged · Nov 17, 2015 · N777FD · Boeing 757222 · Fuselage Main, Frame
  > CABIN STATION 1460, STRINGER 1 FRAME WEB FOUND TWO EACH ELONGATED HOLES AFTER BRACKET REMOVED, REF SNRM N01466. CABIN FRAME REPAIR CARRIED OUT IAW SRM 53-00-07 FIG 201 REPAIR 3 REV 116. THIS IS A CAT B REPAIR WITH A THRESHOLD OF 10,000 FLIGHT CYCLES, AFTER
- [SDR FDEA201511173658](https://openairdocs.org/sdr/FDEA201511173658.md): Frame · damaged · Nov 17, 2015 · N777FD · Boeing 757222 · Fuselage Main, Frame
  > CABIN STATION 1480, STRINGER 1 FRAME TWO EACH FASTENER HOLES FOUND ELONGATED. FRAME REPAIR CARRIED OUT AT STATION 1480, LBL 3 & RBL 3 IAW SRM 53-00-07 FIG 201 REPAIR 3 REV 116. THIS IS A CAT B REPAIR WITH A THRESHOLD OF 10,000 FLIGHT CYCLES, AFTER REPAIR HFE
- [SDR FDEA201511083517](https://openairdocs.org/sdr/FDEA201511083517.md): Support · corroded · Nov 8, 2015 · N777FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > BS 680, RBL 24.75 SEAT TRACK CROWN SUPPORT FOUND CORRODED. REPAIRED IAW EA F-5310-T0321853 A PART 1. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201510313430](https://openairdocs.org/sdr/FDEA201510313430.md): Crease Beam · damaged · Oct 31, 2015 · N777FD · Boeing 757222 · Fuselage Main, Structure
  > CABIN STATION 1110 RT, CREASE BEAM WEB FOUND 01 ELONGATED HOLE. CABIN CREASE BEAM WEB AT STATION 1100 - 1120, RBL 63 & RBL 70.5 REMOVED IAW SRM 51-40-02 REV 116. CREASE BEAM WEB FABRICATED IAW DWG 144N5210 SHT 1 REV. INSTALLED IAW DWG 144N5200 SHT 1 REV B R
- [SDR FDEA201510313429](https://openairdocs.org/sdr/FDEA201510313429.md): Crease Beam · damaged · Oct 31, 2015 · N777FD · Boeing 757200 · Fuselage Main, Structure
  > CABIN STATION 1110 RT, CREASE BEAM INNER CHORD FOUND 01 EACH ELONGATED HOLE. REMOVED IAW SRM 51-40-02 REV 116 FROM STATION 1040 - 1180 RT. CREASE BEAM INNER CHORD FABRICATED IAW DWG 144N5124 SHT 1 REV. INSTALLED IAW 144N5200 SHT 1 REV B & SHT 2 REV B. REPA
- [SDR FDEA201510313428](https://openairdocs.org/sdr/FDEA201510313428.md): Crease Beam · damaged · Oct 31, 2015 · N777FD · Boeing 757222 · Fuselage Main, Structure
  > CABIN STATION 932 RT, CREASE BEAM WEB FOUND O1 EACH ELONGATED HOLE. CREASE BEAM WEB REMOVED AT STATION 920 - 940, RBL 63 & 70.5 IAW SRM 51-40-02 REV 116. CREASE BEAM WEB FABRICATED & INSTALLED IAW DWG 144N5140 SHT 6 REV. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201510313427](https://openairdocs.org/sdr/FDEA201510313427.md): Crease Beam · damaged · Oct 31, 2015 · N777FD · Boeing 757222 · Fuselage Main, Structure
  > CABIN STATION 932 RT, CREASE BEAM INNER CHORD FOUND 01 EACH ELONGATED HOLE. CREASE BEAM INNER CHORD REMOVED AT STATION 900 - 1040 RT IAW SRM 51-40-02 REV 116. CREASE BEAM INNER CHORD FABRICATED IAW DWG 144N5152 SHT 1 REV. INSTALLED IAW DWG 144N5140 SHT 3 RE
- [SDR FDEA201510313426](https://openairdocs.org/sdr/FDEA201510313426.md): Crease Beam · chafed · Oct 31, 2015 · N777FD · Boeing 757222 · Fuselage Main, Structure
  > BS 1590 LT, CREASE BEAM INBD CHORD LOWER SURFACE CHAFED. COMPLIED WITH EA F-5310-T0321812 PART 1. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201510313425](https://openairdocs.org/sdr/FDEA201510313425.md): Crease Beam · corroded · Oct 31, 2015 · N777FD · Boeing 757222 · Fuselage Main, Structure
  > BS 984 - 996 RT, CREASE BEAM INNER CHORD VERTICAL FLANGE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 115. FOUND OUT OF 10% LIMIT IAW SRM 53-40-13 ALLOWABLE DAMAGE 1 REV 116. CREASE BEAM INNER CHORD R & R IAW DWG 144N5140 SHT 3 REV D & SHT 4 RE
- [SDR FDEA201510313424](https://openairdocs.org/sdr/FDEA201510313424.md): Crease Beam · corroded · Oct 31, 2015 · N777FD · Boeing 757222 · Fuselage Main, Structure
  > CABIN STATION 1120 - 1140 LT, CREASE BEAM WEB FOUND CORROSION. FOUND OUT OF 10% LIMIT IAW SRM 53-40-13, ALLOWABLE DAMAGE 1 FIG 101 REV 116. CREASE BEAM WEB REMOVED IAW SRM 51-40-02 REV 116. NEW CREASE BEAM WEB FABRICATED IAW DWG 144N5210 SHT 1 REV. INSTALL
- [SDR FDEA201510313423](https://openairdocs.org/sdr/FDEA201510313423.md): Crease Beam · corroded · Oct 31, 2015 · N777FD · Boeing 757222 · Fuselage Main, Structure
  > CABIN STATION 1420 - 1440 RT, CREASE BEAM WEB UPPER SURFACE CORROSION. CORROSION REMOVED IAW SRM 51-10-02 REV 115. REWORKED AREA EVALUATED, MATERIAL THICKNESS REMOVED 0.010", FOUND OUT OF 10% LIMIT IAW SRM 53-60-13 ALLOWABLE DAMAGE 1 FIG 101 REV 116. CREA
- [SDR FDEA201510313422](https://openairdocs.org/sdr/FDEA201510313422.md): Crease Beam · corroded · Oct 31, 2015 · N777FD · Boeing 757222 · Fuselage Main, Structure
  > CABIN STATION 1140 - 1160 RT, CREASE BEAM WEB FOUND CORROSION. CORROSION REMOVED IAW 51-10-02 REV 115. REWORKED AREA, EVALUATED MATERIAL & REMOVED 0.026" FOUND OUT 10% LIMIT IAW SRM 53-40-13, ALLOWABLE DAMAGE 1 REV 116. CREASE BEAM WEB REMOVED IAW SRM 51-40
- [SDR FDEA201510313421](https://openairdocs.org/sdr/FDEA201510313421.md): Crease Beam · corroded · Oct 31, 2015 · N777FD · Boeing 757222 · Fuselage Main, Structure
  > CABIN STATION 996 - 1020 RT CREASE BEAM WEB FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-02 REV 115. REWORKED EVALUATED MATERIAL & REMOVED 0.014" FOUND OUT OF 10% LIMIT IAW SRM 53-40-12 ALLOWABLE DAMAGE 1 REV 116. CREASE BEAM WEB REMOVED IAW SRM 51-40-0
- [SDR FDEA201510313420](https://openairdocs.org/sdr/FDEA201510313420.md): Beam · cracked · Oct 31, 2015 · N777FD · Boeing 757222 · Fuselage Main, Structure
  > FORWARD E & E COMPARTMENT, STATION 263 BHD, BL 0 VERTICAL BEAM UPPER END CRACKED. CRACKED VERTICAL BEAM REMOVED & NEW VERTICAL BEAM FABRICATED IAW DWG 141N2913 SHT 1 REV B & INSTALLED IAW DWG 141N2910 SHT 1 REV E. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.
- [SDR FDEA201510313419](https://openairdocs.org/sdr/FDEA201510313419.md): Crease Beam · corroded · Oct 31, 2015 · N777FD · Boeing 757222 · Fuselage Main, Structure
  > CABIN STATION 960 - 984 RT CREASE BEAM WEB FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-02 REV 115. REWORKED AREA, EVALUATED MATERIAL THICKNESS, REMOVED 0.020 " FOUND OUT OF 10% LIMITS IAW SRM 53-40-13 ALLOWABLE DAMAGE 1 REV 116. CREASE BEAM WEB R & R I
- [SDR FDEA201510313418](https://openairdocs.org/sdr/FDEA201510313418.md): Crease Beam · corroded · Oct 31, 2015 · N777FD · Boeing 757222 · Fuselage Main, Structure
  > CABIN STATION 940 - 960 RT, CREASE BEAM WEB FOUND CORROSION. REMOVED IAW SRM 51-10-02 REV 116. REWORKED AREA, EVALUATED & REMOVED 0.006" & FOUND OUT OF 10% LIMIT IAW SRM 53-40-13 ALLOWABLE DAMAGE 1 REV 116. CREASE BEAM WEB REMOVED IAW SRM 51-40-02 REV 116.
- [SDR FDEA201510293402](https://openairdocs.org/sdr/FDEA201510293402.md): Skin · damaged · Oct 29, 2015 · N777FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > EXTERIOR SKIN NUMEROUS SMALL NICKS & SCRATCHES ALONG THE BELLY OF THE ACFT, BETWEEN STRINGER 26 LT & 26 RT, AT BS 520 - 540. EXTERIOR SKIN, NUMEROUS SMALL NICKS & SCRATCHES REMOVED, FOUND OUT OF LIMIT AT STATION 537, 2.5" TO STRINGER 28R IAW SRM 53-00-01 FIG
- [SDR FDEA201510283393](https://openairdocs.org/sdr/FDEA201510283393.md): Skin · nicked · Oct 28, 2015 · N777FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN LT SIDE, AFTER SHORING REMOVAL & SKIN CLEAN UP, FOUND A NICK MARK AT BS 620 & STRINGER 28. EXTERIOR SKIN, NICK MARK REMOVED, FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II REV 116. REPAIR CARRIED OUT AS IAW SRM 53-00-01 FIG 201
- [SDR FDEA201510283392](https://openairdocs.org/sdr/FDEA201510283392.md): Skin · scratched · Oct 28, 2015 · N777FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE UNDER SHORING LT SIDE, THERE ARE SEVERAL SMALL SCRATCHES AT THE SHORING PAD AREA, BS 200 - 210, FROM LBL 30 - BL 0. REMOVED & FOUND OUT OF LIMIT AT STATION 200, LBL 9.5 IAW SRM 53-00-01 FIG 101 DETAIL 11 REV 116 & COMPLIED WITH EA F-5330-T0321490 PAR
- [SDR FDEA201510223304](https://openairdocs.org/sdr/FDEA201510223304.md): Seat Track · chafed · Oct 22, 2015 · N777FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN STATION 780 - 790, RBL 45.5, SEAT TRACK CROWN FOUND CHAFED. COMPLIED WITH EA F-5310-T0322310 PART 1. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201510223303](https://openairdocs.org/sdr/FDEA201510223303.md): Seat Track · chafed · Oct 22, 2015 · N777FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN STATION 560 - 564, RBL 24.75, SEAT TRACK CROWN FOUND CHAFED. COMPLIED WITH EA F-5310-T0322362 PART 1. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201510223306](https://openairdocs.org/sdr/FDEA201510223306.md): Seat Track · chafed · Oct 22, 2015 · N777FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN STATION 984 - 996, RBL 24.75, SEAT TRACK CROWN FOUND CHAFED. CHAFED MARK REMOVED IAW SRM 51-10-02 REV 115. REWORKED AREA MEASURED CLEAN UP DEPTH OF 0.028" ON SEAT TRACK CROWN EXCEEDS CROWN LIMIT OF 0.020" IAW SRM 53-00-52 FIG 101 ALLOWABLE DAMAGE 1
- [SDR FDEA201510223305](https://openairdocs.org/sdr/FDEA201510223305.md): Seat Track · chafed · Oct 22, 2015 · N777FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN STATION 780 - 800, RBL 24.75 SEAT TRACK CROWN FOUND CHAFED. CHAFED MARK REMOVED IAW SRM 51-10-02 REV 115. REWORKED AREA, EVALUATED CLEAN UP DEPTH OF 0.493" ON SEAT TRACK, CROWN LIP EXCEED LIP LIMIT OF 0.48" IAW SRM 53-00-52 FIG 101 ALLOWABLE DAMAGE 1 R
- [SDR FDEA201510223302](https://openairdocs.org/sdr/FDEA201510223302.md): Seat Track · chafed · Oct 22, 2015 · N777FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN STATION 700 - 720, RBL 24.75, SEAT TRACK CROWN FOUND CHAFED. CHAFED MARK REMOVED IAW SRM 51-10-02 REV 115. REWORKED AREA, EVALUATED CLEAN UP DEPTH OF 0.028" ON SEAT TRACK CROWN EXCEED CROWN LIMIT 0.02" IAW SRM 53-00-52 FIG 101 ALLOWABLE DAMAGE 1 REV 11
- [SDR FDEA201510193277](https://openairdocs.org/sdr/FDEA201510193277.md): Skin · damaged · Oct 19, 2015 · N777FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN RT SIDE AT BS 1530, BETWEEN STRINGER 27 - 28, THERE IS A DEEP BLEND. DEEP BLEND FOUND OUT OF LIMIT IAW SRM 53-00-01 FIG 101 DETAIL II REV 116 & REPAIR CARRIED OUT IAW SRM 53-00-01 FIG 201 REPAIR 16 REV 116. THIS IS CAT B REPAIR. INSPE
- [SDR FDEA201510193276](https://openairdocs.org/sdr/FDEA201510193276.md): Skin · cracked · Oct 19, 2015 · N777FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > EXTERIOR SKIN NUMEROUS SMALL NICKS & SCRATCHES ALONG THE BELLY OF THE ACFT, BETWEEN STRINGERS 26 LT & 26 RT AT BS 1580 - 1600. REMOVED IAW SRM 51-10-02 REV 115, FOUND WITHIN LIMIT IAW SRM 53-00-01 FIG 101 DETAIL II REV 116, EXCEPT HFEC INSPECTED FOUND CRACK A
- [SDR FDEA201510183271](https://openairdocs.org/sdr/FDEA201510183271.md): Support · corroded · Oct 18, 2015 · N777FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN STATION 365, RBL 45.5 SEAT TRACK CROWN SUPPORT FOUND CORROSION. CABIN STATION 365, RBL 45.5 SEAT TRACK CROWN SUPPORT CORROSION REMOVED IAW SRM 51-10-02 REV 116 & FOUND CORROSION MORE THAN 50% THRU. SEAT TRACK CROWN & SUPPORT REMOVED BETWEEN STATION 365
- [SDR FDEA201510183270](https://openairdocs.org/sdr/FDEA201510183270.md): Support · corroded · Oct 18, 2015 · N777FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN STATION 365, RBL 24.75 SEAT TRACK CROWN SUPPORT FOUND CORROSION. SEAT TRACK CROWN SUPPORT CORROSION REMOVED IAW SRM 51-10-02 REV 116 & FOUND CORROSION MORE THAN 50% THRU. SEAT TRACK CROWN & SUPPORT REMOVED, BETWEEN STATION 365 - 440, RBL 24.75 IAW SRM
- [SDR FDEA201510173264](https://openairdocs.org/sdr/FDEA201510173264.md): Splice · corroded · Oct 17, 2015 · N777FD · Boeing 757200 · Fuselage Main, Structure
  > BS 1080 RT CREASE BEAM INNER CHORD SPLICE FITTING FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-02 REV 115. FOUND CORROSION MORE THAN 50% THROUGH. CORRODED SPLICE FITTING REMOVED IAW SRM 51-40-02 REV 116. SPLICE FITTING FABRICATED IAW DWG 144N5215 SHT 1
- [SDR FDEA201510163254](https://openairdocs.org/sdr/FDEA201510163254.md): Splice · corroded · Oct 16, 2015 · N777FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > BS 1120 RT, CREASE BEAM INNER CHORD SPLICE FITTING, FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-02 REV 115. FOUND MORE THAN 50% THROUGH. CORRODED SPLICE FITTING REMOVED IAW SRM 51-40-02 REV 116. SPLICE FITTING FABRICATED IAW DWG 144N5215 SHT 1 REV & I
- [SDR FDEA201510163253](https://openairdocs.org/sdr/FDEA201510163253.md): Door Sill · corroded · Oct 16, 2015 · N777FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR CUT OUT LOWER SILL WEB, CORROSION AT STATION 1420. AFT CARGO DOOR CUT OUT CORRODED WEB AT STATION 1380 - 1440, STRINGER 27R, R & R WITH NEW FABRICATED WEB IAW DWG 146N8522 SHT 1 REV E. NEW WEB FABRICATED IAW DWG 146N8522 SHT 1 REV E. REPAIR C
- [SDR FDEA201510143204](https://openairdocs.org/sdr/FDEA201510143204.md): Seat Track · chafed · Oct 14, 2015 · N777FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
  > BS 1555 - 1575, RBL 24.75, SEAT TRACK CROWN CHAFED. CHAFE REMOVED IAW SRM 51-10-02 REV 116. REWORKED AREA, AND FOUND OUT OF LIMITS IAW SRM 53-00-52 FIG 101 REV 116. SEAT TRACK REMOVED, & FABRICATED IAW DWG 146N5137 SHT 1 REV & INSTALLED IAW DWG 146N5120 SHT

Next page: https://openairdocs.org/aircraft/N777FD/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 = 'N777FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N777FD/reports

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