# Service difficulty reports: N771FD

A list on [N771FD](https://openairdocs.org/aircraft/N771FD.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 · 56 reports

- [SDR FDEA202207131712](https://openairdocs.org/sdr/FDEA202207131712.md): Warning Message · false activation · Jul 12, 2022 · N771FD · Boeing 757222 · Cabin Pressure Control System
  > CABIN ALTITUDE WARNING DESCENDING THROUGH FLIGHT LEVEL 220. CABIN ALTITUDE WAS 10,100. EMERGENCY DECLARED TO GET AN EXPEDITED DESCENT TO 10,000 FEET. ***EMERGENCY DECLARED*** CHECKED LEFT PACK CONTROLLER FOR FAULTS, NONE FOU
- [SDR FDEA2021083082127](https://openairdocs.org/sdr/FDEA2021083082127.md): Window · sparks · Aug 28, 2021 · N771FD · Boeing 757222 · Windshield/Door Rain/Ice Removal
  > DURING PREFLIGHT, SELECTED WINDOW HEAT SWITCHED ON AND IMMEDIATELY HAD RIGHT SIDE WINDOW PRODUCE LARGE SPARK AND AND BEGIN SMOKING. WINDOW SPIRAL HEAT CORD AND TEST WINDOW HEAT, BOTH ACCOMPLISHED, ALSO REF AMM 30-41-00-5 FOR WINDOW HEAT TEST OK.
- [SDR FDEA202106111500](https://openairdocs.org/sdr/FDEA202106111500.md): Frame · cracked · Jun 11, 2021 · N771FD · Boeing 757222 · Fuselage Main, Frame
  > DURING ROTO PROBE OF OPEN HOLES AT RH BS 1640 PER EO F-5310-E0344602. A CRACK INDICATION WAS NOTED IN THE BOTTOM INBD HOLE. THE CRACK IS IN THE FRAME AT APPROX. 3:00 O'CLOCK. COMPLIED WITH EA F-5310-T0361948 AND COMPLETED ALL STEPS 1-17 FUSELAGE - MAINFR
- [SDR FDEA202106081469](https://openairdocs.org/sdr/FDEA202106081469.md): Floor Panel · delaminated · Jun 8, 2021 · N771FD · Boeing 757222 · Fuselage Floor Panel
  > FLOOR PANEL 222AF IS DELAMINATED FLOOR BOARD 222AF FABRICATED ON TRAVELER # T21/1555539 IAW SRZ-25-005 MAJOR REPAIR
- [SDR FDEA202106081467](https://openairdocs.org/sdr/FDEA202106081467.md): Floor Panel · delaminated · Jun 8, 2021 · N771FD · Boeing 757222 · Fuselage Floor Panel
  > FLOOR PANEL 221AF IS DELAMINATED FLOORBOARD 221AF FABRICATED ON TRAVELER # T21/1555527 IAW DWG SRZ-25-005 MAJOR REPAIR
- [SDR FDEA202104090861](https://openairdocs.org/sdr/FDEA202104090861.md): Proximity Sensor · contaminated · Apr 9, 2021 · N771FD · Boeing 757222 · Door Warning System
  > PASSING 13000 FT IN DESCENT TO KRST, RECEIVED EICAS ALERT L WING SLIDE. EMER DOORS LIGHT ALSO ILLUMINATED ON OVERHEAD PANEL. COMPLIED WITH QRH. NO OTHER UNUSUAL INDICATIONS. PERFORMED BITE TEST ON PROX BOX AND FOUND CODE 373 CONVERTS TO SENSOR S1037
- [SDR FDEA202103210737](https://openairdocs.org/sdr/FDEA202103210737.md): Guide Arm · out of adjust · Mar 21, 2021 · N771FD · Boeing 757222 · Passenger/Crew Doors
  > RAMP REPORTED L1 DOOR WOULD NOT OPEN FULLY. OPENS PARTIALLY AT THE TOP. BOTTOM STAYS ENGAGED. REMOVED FROM MEL STATUS. COMPLETED ADJUSTMENT OF L1 DOOR GUIDE ARM REF. B757 AMM 52-11-04-2, AND DOOR
- [SDR FDEA202101270208](https://openairdocs.org/sdr/FDEA202101270208.md): Module · failed · Jan 27, 2021 · N771FD · Boeing 757222 · Landing Gear Selector
  > AFTER SELECTING LANDING GEAR DOWN "GEAR" AMBER LIGHT ILLUMINATED AND "GEAR DISAGREE" EICAS MESSAGE APPEARED. AFTER SEVERAL SECONDS THE EICAS MESSAGE AND LIGHT BOTH EXTINGUISHED. PERFORMED BITE PROCEDURE ON PSEU PER FIM 32-09 FAULT TREE 802. FAULT CODES AP
- [SDR FDEA201909042098](https://openairdocs.org/sdr/FDEA201909042098.md): Cvr · malfunctioned · Sep 4, 2019 · N771FD · Boeing 757222 · Audio/Video Monitoring
  > WHILE AT CRUISE AT 15,000 FEET FROM KBUF TO KSYR, RECEIVED "MAIN CARGO FIRE" EICAS AND MASTER WARNING. SMOKE FILLED COCKPIT. DECLARED EMERGENCY, RAN QRH, IMMEDIATE DIVERT INTO KROC. FULL STOPPED ON RUNWAY AND EGRESSED AIRCRAFT VIA LEFT SLIDE. REPLACED RECIRC
- [SDR FDEA201909042085](https://openairdocs.org/sdr/FDEA201909042085.md): Unknown · smoke · Sep 4, 2019 · N771FD · Boeing 757222 · Air Distribution System
  > WHILE AT CRUISE AT 15,000 FEET FROM KBUF TO KSYR, RECEIVED "MAIN CARGO FIRE" EICAS AND MASTER WARNING. SMOKE FILLED COCKPIT. DECLARED EMERGENCY, RAN QRH, IMMEDIATE DIVERT INTO KROC. FULL STOPPED ON RUNWAY AND EGRESSED AIRCRAFT VIA LEFT SLIDE. PER FIM 21-00-01-
- [SDR FDEA2019082642012](https://openairdocs.org/sdr/FDEA2019082642012.md): Module · unknown · Aug 24, 2019 · N771FD · Boeing 757222 · Landing Gear Position and Warning
  > RECEIVED RED CONFIGURATION LIGHT, RED GEAR NOT DOWN EICAS MESSAGE, AND WARNING HORN INTERMITTENLY FROM TOP OF DECENT TO 4000 FEET MSL. PERFORMED TROUBLESHOOTING OF LANDING GEAR CONFIGURATION WARNING PROBLEMS IAW FIM 31-51 FAULT TREES 814 AND 817. NO DEFECTS
- [SDR FDEA2019081541896](https://openairdocs.org/sdr/FDEA2019081541896.md): Structure · damaged · Aug 14, 2019 · N771FD · Boeing 757222 · Passenger/Crew Doors
  > FOUND DAMAGE TO L1 DOOR AT UPPER LEFT CORNER INSTALLED REPAIR IAW SRM 52-10-01-2R, AND EA F - 5210-T0348898 PT 1, PAINTED AND SEALED IAW SRM 52-10-01-2R, INSTALLED DOOR LINER AND CONNECTED HANDLE IAW AMM 52-11-02-4.
- [SDR FDEA2019080761802](https://openairdocs.org/sdr/FDEA2019080761802.md): Bottle · empty · Aug 6, 2019 · N771FD · Boeing 757222 · Emergency Equipment
  > ON MAINT PREFLIGHT FOUND L-1 DOOR ASSIST BOTTLE NITROGEN DEPLETED. SLIDE NOT DEPLOYED. R & R L-1 EMERGENCY POWER RESERVIOR IAW MM 52-11-30-4.
- [SDR FDEA2019060651223](https://openairdocs.org/sdr/FDEA2019060651223.md): Skin · damaged · Jun 5, 2019 · N771FD · Boeing 757222 · Wing, Plate/Skin
  > PREVIOUS REPAIR ON TOP OF LEFT HAND WING TIP DISBONDED WS. 780 REMOVED DAMAGED AREA AND PREPARED REPAIR IAW B 757 SRM 57-20-01-2R FIG 201 AND 51- 70-10-2R REPAIR 4 PARAG. 3A AND B,APPLIED FILLER AND DOUBLER REPAIR AT LEFT HAND WING TIP WS 780 IAW B 757 IAW
- [SDR FDEA2019060321207](https://openairdocs.org/sdr/FDEA2019060321207.md): Skin · delaminated · Jun 2, 2019 · N771FD · Boeing 757222 · Wing, Plate/Skin
  > DELAMINATION FOUND ON NO STEP AREA TOP OF LEFT WING TIP EXTERIOR SKIN WSTA. 780. REMOVED DELAMINATION FOR EVAL. IAW B SRM 57-20-01-2R AND 51-70-10,CUT OUT AREA DAMAGED,APPLIED FILLER AND DOUBLER REPAIR AT LEFT EXTERIOR SKIN WSTA 780 IAW SRM 51-70-10-2R FIG
- [SDR FDEA201905181093](https://openairdocs.org/sdr/FDEA201905181093.md): Frame · gouged · May 18, 2019 · N771FD · Boeing 757222 · Fuselage Main, Frame
  > GOUGED FRAME STA 231.25 BL0 IN FORWARD ACCESORY COMPARTMENT. BLENDED GOUGED AREA ON FRAME STA 231.25 BL- 0 IAW SRM 51-10-02-0G, AFTER FURTHER EVALUATION FOUND DAMAGED TO BE OUT OF LIMITS IAW SRM 53-00-07-1A FIG 101 DETAIL II, CUT OUT DAMAGED AREA IAW SRM 53-00
- [SDR FDEA201901070044](https://openairdocs.org/sdr/FDEA201901070044.md): Warning System · false activation · Jan 7, 2019 · N771FD · Boeing 757222 · Landing Gear Position and Warning
  > ON APPROACH WHEN GEAR SELECTED DOWN, SHOWED 3 GREEN BUT WE GOT A GEAR DISAGREE CAUTION MESSAGE AND LIGHT. QRH RAN AND LIGHT EXTENGUISHED. GEAR SHOWED DOWN AND 3 GREEN THE WHOLE TIME. PSEU BITE TEST RESULTS: 067, 094, 090, 086, 083, 421, 422, 423, 424. VERIFY
- [SDR FDEA201707011816](https://openairdocs.org/sdr/FDEA201707011816.md): Life Vest · missing · Jul 1, 2017 · N771FD · Boeing 757222 · Life Jacket
  > ON PREFLIGHT, CAPTAIN/S LPU WAS MISSING. INSTALLED CAPTAINS LIFE VEST AT REAR OF CAPTS SEAT, REF DRAWING B57-25-011. OK FOR SERVICE.
- [SDR FDEA201705311550](https://openairdocs.org/sdr/FDEA201705311550.md): Bulkhead · cracked · May 31, 2017 · N771FD · Boeing 757222 · Fuselage Main, Bulkhead
  > BS 1880, APU FIREWALL, FWD LOWER, RT SIDE, HAS A CRACK. REPAIRED IAW B757 SRM 51-40-02, AND 53-80-08-08-2R.
- [SDR FDEA201705261525](https://openairdocs.org/sdr/FDEA201705261525.md): Frame · corroded · May 26, 2017 · N771FD · Boeing 757222 · Fuselage Main, Frame
  > BS 1640 FRAME, BETWEEN STRINGERS 9 AND 10R HAS CORRODED. REPAIRED THE FRAME IAW EA F-5310-T0333417.
- [SDR FDEA201705231489](https://openairdocs.org/sdr/FDEA201705231489.md): Bulkhead · cracked · May 23, 2017 · N771FD · Boeing 757222 · APU Cowling/Containment
  > BS 1880, APU FIREWALL, FWD, LOWER, RT SIDE, A REPAIR HAS A CRACK. REMOVED THE REPAIR AT BS 1880, ON THE APU FIREWALL IAW SRM 51-40-02. FABRICATED A NEW DOUBLER IAW 53-80-08-2R AND INSTALLED NEW DOUBLER IAW SRM 53-80-08-2R.
- [SDR FDEA201610193655](https://openairdocs.org/sdr/FDEA201610193655.md): Switch · failed · Oct 19, 2016 · N771FD · Boeing 757222 · Drag Control System
  > ON TAKEOFF ROLL, WITH POWER STABILIZED, AT ABOUT 50 KNOTS THE SPOILERS EICAS ALERT AND AUREL WARNING APPEARED. REJECTED TAKEOFF AND ALERT DISAPPEARED AT ABOUT 40 KNOTS. R & R SPEED BRAKE HANDLE POSITION SWITCH IAW MM 31-51-03-4, AND W/D32-42-12. OPS CHEC
- [SDR FDEA201610193654](https://openairdocs.org/sdr/FDEA201610193654.md): Control Module · malfunctioned · Oct 19, 2016 · N771FD · Boeing 757222 · Drag Control System
  > DURING TAKEOFF ROLL AT ABOUT 50 KNOTS, RECEIVED A SPOILERS EICAS MESSAGE AND WARNING TONE. TAKEOFF WAS REJECTED AND SPOILERS EICAS WENT AWAY AS AIRCRAFT REACHED TAXI SPEED ON ABORT. REMOVED AND REPLACED THE SPOILER CONTROL MODULE IAW AMM 27-09-00-2, OPS CH
- [SDR FDEA201608132886](https://openairdocs.org/sdr/FDEA201608132886.md): Slat System · malfunctioned · Aug 13, 2016 · N771FD · Boeing 757222 · Leading Edge Slat Control System
  > AFTER TAKEOFF, RECEIVED A LE SLAT ASYM EICAS MESSAGE AND LEADING EDGE ANUNCIATOR, WHEN FLAPS WERE SELECTED FROM FLAPS 1 TO THE UP POSITION. COMPLIED WITH QRH PROCEDURE, RETUNED TO DEPARTURE. RECONNECTED RT LEADING EDGE SLAT DRIVE COUPLING TO ANGLE GEARBOX
- [SDR FDEA201510063088](https://openairdocs.org/sdr/FDEA201510063088.md): Module · failed · Oct 6, 2015 · N771FD · Boeing 757222 · Landing Gear Selector
  > ON APPROACH, LOWERED THE LG. GEAR DISAGREE EICAS ALERT ALONG WITH CORRESPONDING AMBER GEAR LIGHT. WIGGLED GEAR HANDLE SEVERAL TIME. EICAS & GEAR LIGHT EXTINGUISHED, LANDED SAFELY. R & R THE LANDING GEAR CONTROL LEVER MODULE. OPS CHECKED GOOD IAW AMM 32-3
- [SDR FDEA201505211606](https://openairdocs.org/sdr/FDEA201505211606.md): Skin · dented · May 21, 2015 · N771FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN DENTED AT BS 743, 3" BELOW STRINGER 3L. ACCOMPLISHED EA F-5330-T0315854 PT 1. CROWN SKIN HAS A DENT WITH CREASE, FORM 8110-3 DATED 04 16 15 ATTACHED. THIS IS A CAT B REPAIR, MAJOR REPAIR.
- [SDR FDEA201505171529](https://openairdocs.org/sdr/FDEA201505171529.md): Skin · damaged · May 17, 2015 · N771FD · Boeing 757222 · Trailing Edge Flaps
  > RIGHT INBD FLAP HAS CONTACT DAMAGE, DENT APPROX 1.5" DIAMETER. FINAL REPAIR DIMENSIONS 4.0" DIAMETER, DOUBLER, LOCATED 85.5" FROM MF STATION 300.38 & 21.5 FWD OF TE. REPAIRED RT INBD FLAP UPPER SURFACE IAW SRM 51-70-10.
- [SDR FDEA201505141514](https://openairdocs.org/sdr/FDEA201505141514.md): Skin · damaged · May 14, 2015 · N771FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > SCRIBE LINE DAMAGE AT LAP SEAM 19R, BS 660 - 662. COMPLIED WITH EA F-5330-T0317014 B PT 1. FUSELAGE, PLATE & SKINS, SCRIBE LINE LRTS INSPECTIONS STRINGER 19R, STATION 660.9 - 662.0. MAJOR REPAIR CAT B.
- [SDR FDEA201505141513](https://openairdocs.org/sdr/FDEA201505141513.md): Skin · damaged · May 14, 2015 · N771FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > SCRIBE LINE DAMAGE AT LAP SEAM 14R, BS 530 - 533. COMPLIED WITH EA F-5330-T031688 A PT 1. FUSELAGE, PLATES & SKINS SECTION 43, SCRIBE LINE LRTS INSPECTIONS, STRINGER 14R, BS 530.87 - BS 533.091, 2.21" LG. MAJOR REPAIR CAT B.
- [SDR FDEA201505081417](https://openairdocs.org/sdr/FDEA201505081417.md): Skin · damaged · May 8, 2015 · N771FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > SCRIBE LINE FOUND AT STRINGER 26LT, STATION 1659.7 - 1663.5, DEPTH IS.0015", LENGTH IS 3.80", FWD.02", MID.02", AFT.02", FROM LAP. ACCOMPLISHED EA F-5330-T317267 PT 1. FUSELAGE PLATES & SKINS, SCRIBE LINE LRTS INSPECTIONS. THIS IS A CAT A REPAIR. MAJOR
- [SDR FDEA201504231285](https://openairdocs.org/sdr/FDEA201504231285.md): Skin · corroded · Apr 23, 2015 · N771FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > PITTING CORROSION ON LOWER SKIN AT LAP SEAM 26L, BS 709 - 712. ACCOMPLISHED EA F-5330-T0314641 DATE 04 21 15. FUSELAGE SKIN BLEND REPAIR BS 706 - 712 & STRINGER 26L. THIS IS A CATEGORY A REPAIR. CLASSIFIED MAJOR REPAIR.
- [SDR FDEA201504171252](https://openairdocs.org/sdr/FDEA201504171252.md): Access Panel · chafed · Apr 17, 2015 · N771FD · Boeing 757222 · Wing, Plate/Skin
  > LEFT INBD FLAP UPPER ACCESS PANEL IS CHAFED ON THE UPPER SURFACE. REPAIRED LT INBD FLAP UPPER ACCESS PANEL IAW SRM 51-70-10 REPAIR 4. CLASS A MAJOR REPAIR.
- [SDR FDEA201504161248](https://openairdocs.org/sdr/FDEA201504161248.md): Skin · damaged · Apr 16, 2015 · N771FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > SCRIBE LINE DAMAGE FOUND AT LAP SEAM 14L, BS 767 - 769. COMPLIED WITH EA F-5330-T0315549, PT 1. FUSELAGE SKIN REPAIR BETWEEN BS 760 - 775 & STRINGER 13L - 15L, REV NEW, DATED APRIL 03, 2015. FAA FORM 8100-9 ATTACHED. MAJOR REPAIR CAT B.
- [SDR FDEA201504021141](https://openairdocs.org/sdr/FDEA201504021141.md): Floorbeam · corroded · Apr 2, 2015 · N771FD · Boeing 757222 · Fuselage Main, Floor Beam
  > MDC FLOORBEAM AT STATION 1681, UPPER CHORD UNDERSIDE SURFACES, HAS AREAS WITH CORROSION, AT & AROUND NUTPLATES, LBL 58 - RBL 58. REMOVED DAMAGE IAW SRM 51-10-02. CHECKED LIMITS FOUND AREA AT STATION 1681, RBL 24 TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DE
- [SDR FDEA201504021140](https://openairdocs.org/sdr/FDEA201504021140.md): Floorbeam · corroded · Apr 2, 2015 · N771FD · Boeing 757222 · Fuselage Main, Floor Beam
  > MDC FLOORBEAM AT STATION 1681, UPPER CHORD UNDERSIDE SURFACES, HAS AREAS WITH CORROSION, AT & AROUND NUTPLATES, LBL 58 - RBL 58. REMOVED DAMAGE IAW SRM 51-10-02. CHECKED LIMITS FOUND AREA AT STATION 1681, RBL 24 TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101
- [SDR FDEA201503311126](https://openairdocs.org/sdr/FDEA201503311126.md): Keelbeam · corroded · Mar 31, 2015 · N771FD · Boeing 757222 · Fuselage Main, Keel
  > FORWARD PIT, BS 839 - 860, RT KEEL BEAM EXTENSION CORRODED. REMOVED CORROSION RT KEEL BEAM STATION 839 - 860, STRINGER 28L - 29R IAW SRM 51-10-02. CHECKED LIMITS & FOUND TO BE OUT OF LIMITS IAW SRM 53-30-12 FIG 101 DETAIL 1. COMPLIED WITH EA F-5310-T0315372
- [SDR FDEA201503311125](https://openairdocs.org/sdr/FDEA201503311125.md): Keelbeam · corroded · Mar 31, 2015 · N771FD · Boeing 757222 · Fuselage Main, Keel
  > FORWARD PIT, BS 839 - 860, LT KEEL BEAM EXTENSION CORRODED. REMOVED CORROSION LT KEEL BEAM, STATION 839 - 860, STRINGER 28L - 29R IAW SRM 51-10-02. CHECKED LIMITS, OUT OF LIMITS IAW SRM 53-30-12 FIG 101 DETAIL 1. REPAIRED IAW F-5310-T0315372 PT 1 EA, MAJOR
- [SDR FDEA201503251085](https://openairdocs.org/sdr/FDEA201503251085.md): Structure · cracked · Mar 25, 2015 · N771FD · Boeing 757222 · Nacelle/Pylon Miscellaneous Structure
  > LEFT NACELLE STRUT UPPER SPAR, RT CHORD CRACKED, NACELLE STATION 136. ACCOMPLISHED EA F-5450-T0315257 PT 1. MAJOR REPAIR CAT B.
- [SDR FDEA201503251084](https://openairdocs.org/sdr/FDEA201503251084.md): Bulkhead · chafed · Mar 25, 2015 · N771FD · Boeing 757222 · Nacelle/Pylon, Bulkhead/Firewall
  > LEFT NACELLE STRUT BULKHEAD AFT LOWER LT CORNER SURFACE HAS CHAFED AREA, NACELLE STATION 202. COMPLIED WITH EA F-5450-T0315113 PT 1. AFT BULKHEAD CHAFE REPAIR NACELLE STATION 201.02. MAJOR REPAIR.
- [SDR FDEA201503251083](https://openairdocs.org/sdr/FDEA201503251083.md): Stringer · corroded · Mar 25, 2015 · N771FD · Boeing 757222 · Fuselage Main, Longeron/Stringer
  > AFT PIT STRINGER 19L, STATION 1456, HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. BLENDED AREA NO ALLOWABLE DAMAGE IN THE SRM. R & R STRINGER FROM STATION 1416 - 1456, STRINGER 19L IAW SRM 51-40-02. MAJOR REPAIR.
- [SDR FDEA201503120858](https://openairdocs.org/sdr/FDEA201503120858.md): Skin · delaminated · Mar 12, 2015 · N771FD · Boeing 757222 · Trailing Edge Flaps
  > RIGHT INBD AFT FLAP OTBD UPPER CORNER SKIN HAS DELAMINATION. REPAIRED IAW 51-70-04 PARA 4. MAJOR REPAIR.
- [SDR FDEA201503120857](https://openairdocs.org/sdr/FDEA201503120857.md): Skin · dented · Mar 12, 2015 · N771FD · Boeing 757222 · Trailing Edge Flaps
  > RIGHT INBD FLAP, LOWER SURFACE TE WEDGE HAS THREE DENTS, OTBD OF AFT FLAP 5.5" FROM TE. REPAIRED IAW 51-70-10 REPAIR 4. MAJOR REPAIR.
- [SDR FDEA201503100787](https://openairdocs.org/sdr/FDEA201503100787.md): Stringer Splice · corroded · Mar 10, 2015 · N771FD · Boeing 757222 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT AT STATION 1460, STRINGER 23L, SPLICE IS CORRODED.
- [SDR FDEA201503070718](https://openairdocs.org/sdr/FDEA201503070718.md): Stringer Splice · corroded · Mar 7, 2015 · N771FD · Boeing 757222 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT AT BS 1460, STRINGER SPLICE 21L CORRODED.
- [SDR FDEA201503060705](https://openairdocs.org/sdr/FDEA201503060705.md): Skin · damaged · Mar 6, 2015 · N771FD · Boeing 757222 · Vertical Stabilizer, Plate/Skin
  > VERTICAL STAB SKIN LT SIDE ONE EACH BUTTON HEAD FASTENER INSTALLED. BETWEEN BS 1790 & FSS 245.6. REPAIRED VERTICAL STAB SKIN LH FWD SIDE IAW SRM 51-70-10, PARAGRAPH 19, BS 1790, FSS 245.6. MAJOR REPAIR.
- [SDR FDEA201503060703](https://openairdocs.org/sdr/FDEA201503060703.md): Skin · dented · Mar 6, 2015 · N771FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > AFT LOWER FUSELAGE, TWO EACH DENTS WITH SCRATCHES AT STATION 1394, BETWEEN STRINGER 27R - 28R. ACCOMPLISHED EA F-5330-T0315686, P T 1.
- [SDR CALA2015030493189](https://openairdocs.org/sdr/CALA2015030493189.md): Unknown · smoke · Feb 27, 2015 · N771FD · Boeing 757222 · Air Distribution System
  > SMOKE IN COCKPIT & CABIN AT CLIMB POWER WITH LT PACK RUNNING. TURNING OFF PACK STOPS SMOKE REF SERVICE TIP MM 79-00-95-901. DEFERRED LT PACK IAW MEL 2151A. AIRPLANE SOLD AS IS ON 27 FEB 2014. BUYER WAS AWARE OF THIS ITEM PRIOR TO SALE BEING FINALIZED.
- [SDR FDEA201502250596](https://openairdocs.org/sdr/FDEA201502250596.md): Angle · corroded · Feb 25, 2015 · N771FD · Boeing 757222 · Fuselage Miscellaneous Structure
  > APU AIR INTAKE LOWER CUT OUT FLANGE IS EXFOLIATED. L REMOVE CORROSION FROM 2 EA ANGLES AT APE AIR INTAKE DUCT. LOWER CUT OUT YAW SUM 51-10-02. BLENDED TWO EACH ANGLES ORIGINAL MAT, LOSS.06 INCHES, REMAINING.000", FOUND 2EA. ANGLES OUT OF LIMITS AS PE
- [SDR FDEA201502250595](https://openairdocs.org/sdr/FDEA201502250595.md): Duct · corroded · Feb 25, 2015 · N771FD · Boeing 757222 · APU Core Engine
  > APU AIR INTAKE DUCT FWD CUT OUT FLANGE IS EXFOLIATED. REMOVED CORROSION FROM FWD CUT OUT FLANGE AT APU AIR INTAKE AS PER SRM 51-10-02. BLEND STRAP ORIG. MAT..250", MAT. LOSS.250", REMAINING.000", FOUND OUT OF LIMITS AS PER SRM 53-00-01, FIG. 101, DETAI
- [SDR FDEA201502240587](https://openairdocs.org/sdr/FDEA201502240587.md): Skin · dented · Feb 24, 2015 · N771FD · Boeing 757222 · Fuselage Main, Plate/Skin
  > AFT LOWER FUSELAGE SKIN DENT OUTWARD AT STATION 1730 BETWEEN STRINGER 27L - 28L.

Next page: https://openairdocs.org/aircraft/N771FD/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 = 'N771FD' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N771FD/reports

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