# Service difficulty reports: N571FE, cancelled Mar 2, 2024

A list on [N571FE, cancelled Mar 2, 2024](https://openairdocs.org/deregistered/N571FE-2024-03-02.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 3 · 127 reports

- [SDR FDEA2020061981277](https://openairdocs.org/sdr/FDEA2020061981277.md): Line · broken · Jun 18, 2020 · N571FE · Doug MD1010F · Hydraulic System, Main
  > LEVEL 2 HYD 3 FAIL SYSTEM DOWN TO 0.1 GALLONS. COMPLED WITH QRH PROCEDURES AND EMERGENCY/MANUAL GEAR EXTENSION. FOUND BROKEN HYD LINE BEHIND PANEL 616GB, WILL BEGIN REMOVAL OF 616EB FOR BETTER ACCESS. REMOVED DAMAGED SECTION OF HYDRAULIC LINE AND REPAIRED
- [SDR FDEA2020061981270](https://openairdocs.org/sdr/FDEA2020061981270.md): Line · damaged · Jun 18, 2020 · N571FE · Doug MD1010F · Hydraulic System, Main
  > LEVEL 2 HYD 3 FAIL SYSTEM DOWN TO 0.1 GALLONS. COMPLED WITH QRH PROCEDURES AND EMERGENCY/MANUAL GEAR EXTENSION. REMOVED DAMAGED SECTION OF HYDRAULIC LINE AND REPAIRED IAW AMM 20-10-01-2. RESET LANDING GEAR EMERGENCY EXTENSION HANDLE IAW AMM 32-32-01-2.
- [SDR FDEA201912043168](https://openairdocs.org/sdr/FDEA201912043168.md): Slide · defective · Dec 4, 2019 · N571FE · Doug MD1010F · Passenger/Crew Doors
  > 1 LEFT DOOR SLIDE/RAFT LIGHT REMAINS ON. REMOVED AND REPLACED SLIDE RAFT ASSEMBLY.
- [SDR FDEA201908302046](https://openairdocs.org/sdr/FDEA201908302046.md): Unknown · odor · Aug 30, 2019 · N571FE · Doug MD1010F · Cabin Cooling System
  > A/C PACKS EMIT A STRONG ODOR. OPERATED ALL THE PACKS AND UNABLE TO DETECT ANY ODORS IAW MM 21-53-00-7 A/C OK TO CONTINUE.
- [SDR FDEA2019060651218](https://openairdocs.org/sdr/FDEA2019060651218.md): Switch · malfunctioned · Jun 5, 2019 · N571FE · Doug MD1010F · Pneumatic Indicating System
  > LEVEL 3 ALERT "AIR MANF 3 FAIL" REMOVED & REPLACED #3 WING MANIFOLD FAIL DETECTOR SWITCH IAW MD10 MM36-23-03-4 & 36-23-03-5. RAN #3 ENGINE FOR LEAK TEST OF MANIFOLD SYS 3 PER MD10
- [SDR FDEA201808071944](https://openairdocs.org/sdr/FDEA201808071944.md): Rib · damaged · Aug 7, 2018 · N571FE · Doug MD1010F · Wing, Rib/Bulkhead
  > DURING EXTENSION OF THE INBD SLATS, DROOPED SLAT CONTACTED PANEL 616EB, CAUSING DAMAGE TO PANEL AND RIB. REMOVED AND REPLACED THE NUT PLATE STRIP IAW SRM 51-30-01. CUT OUT DAMAGE ON THE FORMER IAW SRM 57-00-01, STEP 20, FIG. 10. INSTALLED A REPAIR IAW SRM
- [SDR FDEA201709142561](https://openairdocs.org/sdr/FDEA201709142561.md): Slide · damaged · Sep 14, 2017 · N571FE · Doug MD1010F · Escape Slide
  > DURING WALK AROUND POST FLIGHT CHECK L1 DOOR WAS INADVERTENLY ARMED AND SLIDE ACCIDENTLY FELL OUT. REMOVED AND REPLACED L1 DOOR SLIDE IAW AMM 25-61-01-2-4, A/C OK FOR SERVICE.
- [SDR FDEA201709142560](https://openairdocs.org/sdr/FDEA201709142560.md): Bottle · low pressure · Sep 14, 2017 · N571FE · Doug MD1010F · Passenger/Crew Doors
  > L1 DOOR AIR BOTTLE REQUIRES SERVICE. SERVICED L1 DOOR AIR RESERVOIR BOTTLE IAW M/M 52-10-01-2. A/C OK FOR SERVICE.
- [SDR FDEA201606081891](https://openairdocs.org/sdr/FDEA201606081891.md): Light · inoperative · Jun 8, 2016 · N571FE · Doug MD1010F · Emergency Equipment
  > L1 DOOR REMOTE SLIDE PRESSURE LIGHT IS INOPERATIVE. RELAMPED LIGHT ASSY IAW SMP. ACFT OK FOR SERVICE.
- [SDR FDEA201606081890](https://openairdocs.org/sdr/FDEA201606081890.md): Indicator · inoperative · Jun 8, 2016 · N571FE · Doug MD1010F · Emergency Equipment
  > L1 DOOR REMOTE SLIDE PRESSURE LIGHT IS INOPERATIVE. RELEASED FOR SERVICE IAW MEL: 25-61-01. EVAC SLIDE REMOTE PRESS INDICATOR INOPERATIVE IAW MEL 25-61-01, VERIFY AND RECORD IN THE AML, EVAC SLIDE SYS PRESSURE, ONCE EACH FLIGHT DAY.
- [SDR FDEA201606031797](https://openairdocs.org/sdr/FDEA201606031797.md): Valve · failed · Jun 3, 2016 · N571FE · Doug MD1010F · Fuel Dump System
  > AFTER FUEL DUMP LT DUMP VALVE FAILED IN OPEN POSITION. R & R FUEL DUMP VALVE IAW 28-30-02. OPERATIONS & LEAK CHECK GOOD.
- [SDR FDEA201605311767](https://openairdocs.org/sdr/FDEA201605311767.md): Skin Panel · dented · May 31, 2016 · N571FE · Doug MD1010F · Wing, Plate/Skin
  > LEFT WING, TOP OTBD TE PANEL BETWEEN SPOILER 4 & 5, APPROX STATION XW619 & XW692. R & R SKIN PANEL IAW EA T8-5720-T-0325706 P1.
- [SDR FDEA201605291752](https://openairdocs.org/sdr/FDEA201605291752.md): Smoke Detector · failed · May 29, 2016 · N571FE · Doug MD1010F · Smoke Detection
  > CENTER CARGO AFT SMOKE DETECTOR FAILED. TEST REPLACED LOWER CTR CARGO SMOKE DETECTOR IAW AMM 26-14-01-4. PERFORMED CARGO SMOKE DETECTOR OPERATIONS TEST IAW AMM 26-14-01-5. OPERATIONS CHECKED GOOD.
- [SDR FDEA201605271746](https://openairdocs.org/sdr/FDEA201605271746.md): Placard · damaged · May 27, 2016 · N571FE · Doug MD1010F · Placards and Markings
  > MAIN DECK FLOOR, FWD BALL MAT AREA FROM BS 608 - 792, LT SIDEWALL TO RT SIDEWALL, DECALS FOR CARGO LOADING PART NUMBERS & LOCATION REFERENCE ARE EITHER WORN, DAMAGED OR ERODED, 2016-05-27. CREATED TO ADD INFO TO SDR 16-1654. R & R DAMAGED PLACARDS IAW DWG 81
- [SDR FDEA201605271744](https://openairdocs.org/sdr/FDEA201605271744.md): Bulkhead · cracked · May 27, 2016 · N571FE · Doug MD1010F · Fuselage Main, Bulkhead
  > RIGHT STATION 595, BULKHEAD WEB HAS APPROX.500 CRACK AT LONGERON 43R, 2016-05-27. REMOVED DAMAGED AREA, FABRICATED FILLER, DOUBLER & FINGER DOUBLER & INSTALLED IAW SRM 51-40-00 FIG 25 VOL 1 & EA 8-5310-T0324747.
- [SDR FDEA201605271743](https://openairdocs.org/sdr/FDEA201605271743.md): Bulkhead · cracked · May 27, 2016 · N571FE · Doug MD1010F · Fuselage Main, Bulkhead
  > RIGHT STATION 595, BULKHEAD WEB HAS APPROX.500 CRACK AT LONGERON 39R, 2016-05-27. REMOVED DAMAGED AREA, FABRICATED FILLER & DOUBLER, INSTALLED IAW SRM 51-40-00 FIG 25 & EA 8-5310-T0-324747.
- [SDR FDEA201605221715](https://openairdocs.org/sdr/FDEA201605221715.md): Skin · cracked · May 22, 2016 · N571FE · Doug MD1010F · Nacelle/Pylon, Plate/Skin
  > NUMBER 2 PYLON AFT FAIRING, BOAT TAIL, RT SIDE HAS MULTIPLE CRACKS IN SKIN CTR SECTION AREA. REPAIRED IAW SRM 54-20-00 FIG 9 VOL 1 & SRM 57-00-01 FIG 4, SHEET 2 VOL 1.
- [SDR FDEA201605221714](https://openairdocs.org/sdr/FDEA201605221714.md): Skin · cracked · May 22, 2016 · N571FE · Doug MD1010F · Nacelle/Pylon, Plate/Skin
  > NUMBER 2 PYLON AFT FAIRING, BOAT TAIL, RT SIDE HAS MULTIPLE CRACKS IN SKIN CTR SECTION AREA. REPAIRED IAW SRM 54-20-00 FIG 9 VOL 1.
- [SDR FDEA201605181655](https://openairdocs.org/sdr/FDEA201605181655.md): Skin · cracked · May 18, 2016 · N571FE · Doug MD1010F · Wing, Plate/Skin
  > LEFT WING PYLON LE, LOWER OTBD SURFACE IS CRACKED. INSTALLED DOUBLER & FILLER IAW EA 8-5710-T0325368.
- [SDR FDEA201605181654](https://openairdocs.org/sdr/FDEA201605181654.md): Seat Track · damaged · May 18, 2016 · N571FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK DAMAGED AT STATION 755, RBL 8 R & R DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL 1.
- [SDR FDEA201605151585](https://openairdocs.org/sdr/FDEA201605151585.md): Angle · cracked · May 15, 2016 · N571FE · Doug MD1010F · Wing Miscellaneous Structure
  > LEFT WING, LT FUELING STATION DOOR, OTBD LANDING IS CRACKED. REPAIRED CRACK IAW SRM 57-00-01 FIG 140.
- [SDR FDEA201605131579](https://openairdocs.org/sdr/FDEA201605131579.md): Tee Fitting · cracked · May 13, 2016 · N571FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > RIGHT STATION 595, BULKHEAD TEE CAP VERTICAL FLANGE AT LONGERON 43R, HAS A 2 INCH CRACK. REPAIRED THE RT STA 595 BULKHEAD TEE CAP AT LONGERONS 39R AND 43R IN REF TO EA 8-5310-T0324747.
- [SDR FDEA201605131577](https://openairdocs.org/sdr/FDEA201605131577.md): Tee Fitting · cracked · May 13, 2016 · N571FE · Doug MD1010F · Fuselage Main, Bulkhead
  > RIGHT STATION 595, BULKHEAD TEE CAP VERTICAL FLANGE AT LONGERON 39R, HAS A 2 INCH CRACK. REPAIRED TEE CAP IN REF TO EA 8-5310-T0324747
- [SDR FDEA201605051473](https://openairdocs.org/sdr/FDEA201605051473.md): Panel · delaminated · May 5, 2016 · N571FE · Doug MD1010F · Wing Miscellaneous Structure
  > RIGHT MAIN WW PANEL ARC 0269-504 IS DELAMINATED, AREA MARKED NR 15 ON BOTTOM SIDE OF PANEL. REPAIRED IAW SRM 51-71-00 VOL II & PREPPED. PAINTED IAW SRM 51-21-02.
- [SDR FDEA201604221351](https://openairdocs.org/sdr/FDEA201604221351.md): Skin · damaged · Apr 22, 2016 · N571FE · Doug MD1010F · Air Conditioning Doors
  > NUMBER 2 ACM DOOR, LOWER FWD CORNER DAMAGED. REPAIRED DOOR IAW DPS 3.69-5 & SRM 52-00-01 VOL 1 FIG 4 SHEET 2.
- [SDR FDEA201604211332](https://openairdocs.org/sdr/FDEA201604211332.md): Seat Track · corroded · Apr 21, 2016 · N571FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO COMPARTMENT, FOUND EXFOLIATION CORROSION ON THE NR 3 SEAT TRACK AT STATION 1841 - 1877, RBL 30R. R & R SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1A SHEET 7.
- [SDR FDEA201604201313](https://openairdocs.org/sdr/FDEA201604201313.md): Former · cracked · Apr 20, 2016 · N571FE · Doug MD1010F · Horizontal Stabilizer, Spar/Rib
  > RIGHT HORIZONTAL STABILIZER INBD, LE FIXED SEGMENT HAS A 1" CRACK AT THE NOSE RIB LOWER AFT CORNER, EMANATING FROM ONE FASTENER TO THE EDGE OF THE NEXT, JUST INBD OF THE REMOVED LE SECTION, APPROX STATION XFS 88.83. REMOVED DAMAGED LE FORMER, INSTALLED LE FO
- [SDR FDEA201604191281](https://openairdocs.org/sdr/FDEA201604191281.md): Finger Doubler · cracked · Apr 19, 2016 · N571FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > CAC FINGER DOUBLER CORRODED & CRACKED AT SPLICE STATION 1129, MARKED OTBD OF LONGERON 48L. REPAIR IAW SRM 53-20-00 FIG 6.
- [SDR FDEA201604191280](https://openairdocs.org/sdr/FDEA201604191280.md): Floorboard · damaged · Apr 19, 2016 · N571FE · Doug MD1010F · Fuselage Floor Panel
  > FORWARD CARGO BAY FLOORBOARD AT STATION 735, LBL 20, HAS A DAMAGED CORNER & NEEDS TO BE REPLACED. FABRICATED A NEW FLOORBOARD IAW SRZ-25-005.
- [SDR FDEA201604191279](https://openairdocs.org/sdr/FDEA201604191279.md): Floorboard · damaged · Apr 19, 2016 · N571FE · Doug MD1010F · Fuselage Floor Panel
  > FORWARD CARGO PIT FLOORBOARD PANEL AT STATION 959, LBL 70, HAS A DAMAGED CORNER & NEEDS TO BE REPLACED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005.
- [SDR FDEA201604171240](https://openairdocs.org/sdr/FDEA201604171240.md): Skin Panel · cracked · Apr 17, 2016 · N571FE · Doug MD1010F · Horizontal Stabilizer, Plate/Skin
  > RIGHT UPPER AFT HORIZONTAL STABILIZER SKIN PANEL INBD AFT CORNER HAS A.400 INCH CRACK. CRACK STOP DRILLED IAW WC 55X1203ALI-P4 FIGURE 2 TABLE 1. CRACK FOUND TO BE LIMITS. TRACKING TO BE ACCOMPLISHED ON WC AT 80 FLIGHT HOUR INTERVALS.
- [SDR FDEA201604131205](https://openairdocs.org/sdr/FDEA201604131205.md): Spar Cap · cracked · Apr 13, 2016 · N571FE · Doug MD1010F · Wing Spar
  > RIGHT WING REAR SPAR LOWER CAP, CRACK LOCATED AT STATION XORS 412. CRACK STARTS ON AFT EDGE & CONTINUES ALONG HORIZONTAL AFT FLANGE THRU ONE BOLT HOLE FWD INTO RADIUS. CRACK IS APPROX 1.5 INCHES IN LENGTH. REPAIRED RT AFT, LOWER REAR SPAR CAP CRACK IAW EA 8-
- [SDR FDEA201604091315](https://openairdocs.org/sdr/FDEA201604091315.md): Panel · delaminated · Apr 9, 2016 · N571FE · Doug MD1010F · Wing Miscellaneous Structure
  > LEFT WING, PANEL 541JB HAS A DENT & IS DELAMINATING AT THE CORNER. REPAIRED LT WING PANEL 541JB IAW SRM 51-71-00 VOL 2.
- [SDR FDEA201604091207](https://openairdocs.org/sdr/FDEA201604091207.md): Skin · dented · Apr 9, 2016 · N571FE · Doug MD1010F · Trailing Edge Flaps
  > RIGHT WING INBD FLAP, LOWER SURFACE AT STATION XIFH 253, THERE IS A DENT. REPAIRED IAW SRM 57-00-01 FIG 4 SHT 2 SRC TRACKING 8-5750-T0324796.
- [SDR FDEA201604091206](https://openairdocs.org/sdr/FDEA201604091206.md): Skin · dented · Apr 9, 2016 · N571FE · Doug MD1010F · Trailing Edge Flaps
  > RIGHT WING INBD FLAP, LOWER SURFACE AT STATION XIFH 245, THERE IS A DENT. REPAIRED IAW SRM 57-00-01 FIG 4 SHT 2 SRC TRACKING 8-5750-T0324796.
- [SDR FDEA201502270611](https://openairdocs.org/sdr/FDEA201502270611.md): Bottle · low pressure · Feb 27, 2015 · N571FE · Doug MD1010F · Passenger/Crew Doors
  > R1 DOOR PNEUMATIC EMER ASSIST BOTTLE PRESS LOW ON PREFLIGHT. SERVICED R1 DOOR AIR RESERVOIR.
- [SDR FDEA201408162188](https://openairdocs.org/sdr/FDEA201408162188.md): Stanchion · corroded · Aug 16, 2014 · N571FE · Doug MD1010F · Fuselage Main, Attach Fittings
  > AFT CARGO COMPARTMENT STANCHION FOUND WITH CORROSION AT STATION 1781 X=10 RT LOWER SECTION. AFT CARGO COMPARTMENT STANCHION FOUND WITH CORROSION AT STA 1781 X= -10 (RT) REMOVED AND REPLACED WITH FABRICATED STANCHION AS PER SRM 51-31-01 VOLUME II REVISION 1
- [SDR FDEA201408162183](https://openairdocs.org/sdr/FDEA201408162183.md): Fitting · corroded · Aug 16, 2014 · N571FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > LOWER CTR CARGO COMPARTMENT BILGE AREA STA=1721 X=5 SHEAR CLIP SURFACE FOUND WITH MINOR CORROSION. CORROSION ON SHEAR CLIP AT LOWER CENTER CARGO COMPARTMENT BILGE AREA STATION Y=1721, X=5 REMOVED AS PER SRM 51-31-01 VOLUME II REVISION 101. NEW SHEAR CLIP FA
- [SDR FDEA201408162187](https://openairdocs.org/sdr/FDEA201408162187.md): Fitting · corroded · Aug 16, 2014 · N571FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT SHEAR CLIP ANGLE, TWO EACH, AT STATION 1821 BETWEEN L51L TO L51R BILGE AREA FOUND WITH SURFACE CORROSION. CORROSION ON SHEAR CLIP 02 EACH AT AFT CARGO COMPARTMENT STA 1821 BETWEEN LONGERON 51L TO LONGERON 51R REMOVED AS PER SRM 51-31-0
- [SDR FDEA201408162185](https://openairdocs.org/sdr/FDEA201408162185.md): Fitting · corroded · Aug 16, 2014 · N571FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > LOWER CTR CARGO COMPARTMENT BILGE AREA AT STATION Y=1781 X=-5 SHEAR CLIP SURFACE FOUND MINOR CORROSION. CORRODED SHEAR CLIP AT LOWER CENTER CARGO COMPARTMENT BILGE AREA STA Y= 1781, X= -5 REMOVED AS PER SRM 51-31-01 VOLUME II REVISION 101. NEW SHEAR CLIP F
- [SDR FDEA201408162189](https://openairdocs.org/sdr/FDEA201408162189.md): Fitting · corroded · Aug 16, 2014 · N571FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > LOWER FWD CARGO COMPARTMENT BILGE AREA AT STATION = 939 X = 5 SHEAR CLIP SURFACE FOUND MINOR CORROSION. CORRODED SHEAR CLIP AT LOWER FORWARD CARGO COMPARTMENT BILGE AREA AT STA=939, X=5 REMOVED AS PER SRM 51-31-01 VOLUME II REVISION 101. NEW SHEAR CLIP FABRI
- [SDR FDEA201408162186](https://openairdocs.org/sdr/FDEA201408162186.md): Fitting · corroded · Aug 16, 2014 · N571FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > LOWER CTR CARGO COMPARTMENT BILGE AREA AT STATION =1776 X=-35 SHEAR CLIP SURFACE FOUND MINOR CORROSION. CORRODED SHEAR CLIP AT LOWER CENTER CARGO BILGE AREA STA=1776, X=-35 REMOVED AS PER SRM 51-31-01 VOLUME II REVISION 101. NEW SHEAR CLIP FABRICATED AS PER
- [SDR FDEA201408162184](https://openairdocs.org/sdr/FDEA201408162184.md): Fitting · corroded · Aug 16, 2014 · N571FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > LOWER CTR CARGO COMPARTMENT BILGE AREA AT STATION Y=1741 X=5 SHEAR CLIP SURFACE FOUND MINOR CORROSION. CORROSION AT LOWER CENTER CARGO COMPARTMENT BILGE AREA SHEAR CLIP STA Y=1741, X=5 REMOVED AS PER SRM 51-31-01 VOLUME II REVISION 101. NEW SHEAR CLIP FA
- [SDR FDEA201408162182](https://openairdocs.org/sdr/FDEA201408162182.md): Fitting · corroded · Aug 16, 2014 · N571FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > LOWER CTR CARGO COMPARTMENT BILGE AREA AT STATION Y=1761 X= 5 SHEAR CLIP SURFACE FOUND WITH MINOR CORROSION. CORROSION ON SHEAR CLIP AT LOWER CENTER CARGO COMPARTMENT BILGE AREA STA Y=1761 X= 5 REMOVED AS PER SRM 51-31-01 VOLUME II REVISION 101. NEW SHEAR
- [SDR FDEA201408162181](https://openairdocs.org/sdr/FDEA201408162181.md): Fitting · corroded · Aug 16, 2014 · N571FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > LOWER CARGO COMPARTMENT BILGE AREA AT STATION Y= 1761 X= -25 SHEAR CLIP SURFACE FOUND WITH MINOR CORROSION. CORRODED SHEAR CLIP AT LOWER CENTER CARGO COMPARTMENT BILGE AREA AT STA Y=1621, X=-25 REMOVED AS PER SRM 51-31-01 VOLUME II REVISION 101. NEW SHEAR CL
- [SDR FDEA201408082117](https://openairdocs.org/sdr/FDEA201408082117.md): Door Frame · cracked · Aug 8, 2014 · N571FE · Doug MD1010F · Fuselage Main, Structure
  > MAIN DECK R3 DOOR FORWARD JAMB BOX LOWER WEB FOUND CRACKED ON EXISTING REPAIR. AREA CRACKED EXISTING REPAIR DOUBLER AT MAIN DECK R3 DOOR JAMB REMOVED AS PER SRM 51-31-01 VOLUME II REVISION 101. NEW REPAIR DOUBLER FABRICATED AND ACCOMPLISHED REPAIR AS PER SRM
- [SDR FDEA201408082116](https://openairdocs.org/sdr/FDEA201408082116.md): Skin · cracked · Aug 8, 2014 · N571FE · Doug MD1010F · Wing, Plate/Skin
  > DUE TO EXISTING REPAIR DOUBLER REMOVED FOR ACCESS, FOUND CRACK AT LT WING FIXED LEADING SKIN XOS 906. CRACK SKIN AT LEFT HAND WING FIXED LEADING SKIN XOS 906 CARRIED OUT REPAIR AS PER EA 8-5730-T0310420 P1 TITLE (WINGS - PLATES AND SKINS - LT WING - FIXED LE
- [SDR FDEA201408062085](https://openairdocs.org/sdr/FDEA201408062085.md): Hinge Fitting · corroded · Aug 6, 2014 · N571FE · Doug MD1010F · Trailing Edge Flaps
  > LEFT WING INBD FLAP OTBD FWD HINGE BRACKET PIVOT BORE FOUND MINOR SURFACE CORROSION. REWORKED AND FOUND EXCEED LIMITS AS PER CMM 57-44-07 REVISION 62. EXISTING HOLE DIAMETER = 2.554 INCHES. FINAL HOLE DIAMETER = 2.5625 INCHES. MAXIMUM ALLOWABLE DIAMETER =
- [SDR FDEA201408062084](https://openairdocs.org/sdr/FDEA201408062084.md): Floor Support · cracked · Aug 6, 2014 · N571FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT WEB FLOOR SUPPORT AT STATION 1900 X=18 LT CRACKED & CORRODED. FLOOR SUPPORT BEAM (WEB) TRIMMED AND REMOVED AS PER SRM 53-00-01 FIGURE 8 VOLUME I REVISION 101. REPAIR CHANNEL AND FILLER FABRICATED AND INSTALLED AS PER SRM 53-00-01 FIGUR
- [SDR FDEA201408062083](https://openairdocs.org/sdr/FDEA201408062083.md): Frame · corroded · Aug 6, 2014 · N571FE · Doug MD1010F · Fuselage Main, Frame
  > LOWER CARGO COMPARTMENT BILGE AREA AT STATION Y=1781 X=16 FRAME ANGLE FOUND CORROSION. ACCOMPLISHED REPAIR AS PER SRM 53-30-00 FIGURE 5 VOLUME I REVISION 101. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 122. TO PERFORM INITIAL INSPECTION AT 12,000 F

Next page: https://openairdocs.org/deregistered/N571FE-2024-03-02/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 = 'N571FE' AND deregistration_id = 'N571FE-2024-03-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N571FE-2024-03-02/reports

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