# Service difficulty reports: N562FE, cancelled Mar 2, 2024

A list on [N562FE, cancelled Mar 2, 2024](https://openairdocs.org/deregistered/N562FE-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 4 · 178 reports

- [SDR FDEA202011112832](https://openairdocs.org/sdr/FDEA202011112832.md): Skin · cracked · Nov 11, 2020 · N562FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > FWD CARGO DOOR CUT OUT, AFT LOWER CORNER, SKIN HAS MINOR GOUGES ON EDGE OF REPAIR. REPAIRED LOWER AFT CORNER OF FWD CARGO DOOR FRAME, REF SRM 53-50-00 FIGURE 26 SHEETS 2, 3, 4, 5, AND 9 VOL 1 REF SRM 53-50-00 FIGURE 27 SHEET 2 VOL 1. SRM 51-31-01 VOL 2 SRM 5
- [SDR FDEA202011022761](https://openairdocs.org/sdr/FDEA202011022761.md): Skin · corroded · Nov 2, 2020 · N562FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > CORROSION DISCOVERED ON LEFT SIDE FUSELAGE SKIN UNDER LONGERON 46L AT STA BS 1957 TO BS 1961.
- [SDR FDEA202011022747](https://openairdocs.org/sdr/FDEA202011022747.md): Longeron · corroded · Nov 2, 2020 · N562FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > AFT CARGO, APPROXIMATELY STA 1967, SECTION OF LONGERON L46 IS EXFOLIATED OUT OF LIMITS.
- [SDR FDEA202011012744](https://openairdocs.org/sdr/FDEA202011012744.md): Longeron · corroded · Nov 1, 2020 · N562FE · Doug MD1010F · Fuselage Main, Longeron/Stringer
  > LOWER FUSELAGE EXT SKIN HAS RIVET SHEARED STA 1967 L46L, FOUND LONG L46 EXFOLIATED.
- [SDR FDEA202010182552](https://openairdocs.org/sdr/FDEA202010182552.md): Vane · delaminated · Oct 18, 2020 · N562FE · Doug MD1010F · Trailing Edge Flaps
  > LT OUTBOARD FLAP VANE HAS DELAMINATION UNDER NR 5 RUBSTRIP. REPAIRED LT OUTBOARD FLAP VANE DELAMINATION UNDER NR 5 RUBSTRIP AS REQUIRED, REF SRM 57-00-01 AND 51-71-00. MAJOR REPAIR/WINGS-FLIGHT SURFACES-RSC TRACKING EA FOR LT 8-57 50-T0357401. PERFORMED LT
- [SDR FDEA202010132496](https://openairdocs.org/sdr/FDEA202010132496.md): Skin · worn · Oct 13, 2020 · N562FE · Doug MD1010F · Wing, Plate/Skin
  > REWORK SNRM 820 LT WING: DROOP LEADING EDGE OUTBOARD EDGE HAS WEAR MARKS AND DOUBLER IS WORN THROUGH, MARKED AND DOT 44. DISCREPANCY IS A MAJOR REPAIR, PER GMM-06-2-100 AND SRM 51-90-01 VOL 2. REQUIRES SDR, RDR, AND ALL FABRICATION PROCESSES AS REQUIRED. LT
- [SDR FDEA202010112766](https://openairdocs.org/sdr/FDEA202010112766.md): Hinge · corroded · Oct 11, 2020 · N562FE · Doug MD1010F · Trailing Edge Flaps
  > LT WING, OUTBOARD FLAP, INBOARD HINGE HAS CORROSION ON UPPER INBOARD VALLEY. REMOVED CORROSION FROM WEB AREA SURFACE, PER WINGS-ATTACH FITTINGS-LT WING OUTBOARD FLAP INBOARD HINGE-REWORK EA 8-5740-T0357670 PART 1 (P1).
- [SDR FDEA202010112568](https://openairdocs.org/sdr/FDEA202010112568.md): Bracket · cracked · Oct 11, 2020 · N562FE · Doug MD1010F · Leading Edge Devices
  > LT WING LEADING EDGE NR 2 SLAT COVER BRACKET OUTBOARD FWD SECTION CRACKED, MARKED. FABRICATED A NEW SLAT COVER BRACKET P/N ARB1379-11, PER DOUGLAS DWG ARB1379 R R. NR 2 LT SLAT COVER BRACKET, IAW SRM 51-31-01 VOL 2 "MINOR REPAIR"
- [SDR FDEA202010112678](https://openairdocs.org/sdr/FDEA202010112678.md): Panel · damaged · Oct 11, 2020 · N562FE · Doug MD1010F · Wing, Plate/Skin
  > RT WING: DROOP LEADING EDGE OUTBOARD SIDE/EDGE, DOUBLER AND FASTENER ARE WORN/CUT INTO. REPAIRED THE RT DROOP LEADING EDGE, IN REF TO SRM 57-10-00 FIG 97, PAGE 414.
- [SDR FDEA202010112495](https://openairdocs.org/sdr/FDEA202010112495.md): Bracket · cracked · Oct 11, 2020 · N562FE · Doug MD1010F · Leading Edge Devices
  > LT NR 4 SLAT TRACK LEADING EDGE COVER PLATE HAS A CRACKED LT BRACKET. REMOVED AND REPLACED CRACKED LT BRACKET ON LT NR 4 SLAT TRACK LEADING EDGE COVER PLATE, REF SRM 51-31-01 VOL II.
- [SDR FDEA202010102569](https://openairdocs.org/sdr/FDEA202010102569.md): Skin · worn · Oct 10, 2020 · N562FE · Doug MD1010F · Nacelle/Pylon, Plate/Skin
  > NR 2 ENGINE RT SIDE, APPROXIAMTELY STA YTN 133, 6 O`CLOCK POSITION, GOUGED METAL ON FWD RT FAN COWL LAND. MARKED DOT NR 46 REPAIRED, PER SRM 54-10-00 FIG 20 VOL I.
- [SDR FDEA202010102523](https://openairdocs.org/sdr/FDEA202010102523.md): Door Frame · gouged · Oct 10, 2020 · N562FE · Doug MD1010F · Nacelle/Pylon, Main Frame
  > NR 2 ENGINE LT SIDE, APPROXIMATELY STA YTN 133, 6 O`CLOCK POSITION, GOUGED METAL ON FWD LT FAN COWL LAND. MARKED DOT NR 45. REMOVED GOUGED DOOR JAM & REPLACED WITH FABRICATED DOOR JAM, REF SRM 51-31-01, DWG AJC 7415.
- [SDR FDEA202010072560](https://openairdocs.org/sdr/FDEA202010072560.md): Panel · corroded · Oct 7, 2020 · N562FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > AFT FUS ENGINE 2 AREA RT SIDE PANEL (364CR) HAS LIGHT SURFACE CORROSION AROUND HOLES ON A/C SIDE AND INSIDE PANEL, MARKED. 0005202341: ROLON, JUAN M - 19-OCT-2020 03:57. CLEANED LIGHT (MILD) SURFACE CORROSION AROUND HOLES AT 364CR PANEL, INSIDE & A/C SIDE.
- [SDR FDEA202010032429](https://openairdocs.org/sdr/FDEA202010032429.md): Cargo Track · corroded · Oct 3, 2020 · N562FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO, CORROSION ON SEAT TRACK AT FLOORBOARD ATTACH POINTS STA 1801-STA 1841 LBL 24, MARKED NR 8. REMOVED AND REPLACED SECTION OF SEAT TRACK, IN REF TO SRM 52-70-00 FIG 1A.
- [SDR FDEA202010032480](https://openairdocs.org/sdr/FDEA202010032480.md): Floor Support · cracked · Oct 3, 2020 · N562FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > AFT CARGO, CORROSION AND CRACKS ON FLOOR SUPPORT BRACKET AT INBOARD AND OUTBOARD ENDS AT FWD BULKHEAD STA 1781 RBL 16, MARKED NR 4. REPAIRED THE AFT CARGO FLOOR SUPPORT BRACKET, IN REF TO DWG AFA7831 & SRM 51-31-01 VOL 2.
- [SDR FDEA202010032476](https://openairdocs.org/sdr/FDEA202010032476.md): Floor Support · corroded · Oct 3, 2020 · N562FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > AFT CARGO, CORROSION AND CRACKS ON FLOOR SUPPORT BRACKET AT INBOARD AND OUTBOARD ENDS AT FWD BULKHEAD STA 1781 LBL 25, MARKED NR 2. REPAIRED THE FLOOR SUPPORT, IN REF TO DWG AFA7831 & SRM 51-31-01 VOL 2.
- [SDR FDEA202010012767](https://openairdocs.org/sdr/FDEA202010012767.md): Hinge · corroded · Oct 1, 2020 · N562FE · Doug MD1010F · Trailing Edge Flaps
  > LT OUTBOARD FLAP INBOARD HINGE AIRCRAFT SIDE, ACTUATOR ATTACH LUG RUSTED AT BASE ON BOTH SIDE. LT OUTBOARD FLAP INBOARD HINGE A/C SIDE CORROSION ON ACTUATOR ATTACH LUG WEB BASE WAS REPAIRED PER EA, WINGS ATTACH FITTING LT WING OUTBOARD FLAP INBOARD HINGE EA 8
- [SDR FDEA202010012667](https://openairdocs.org/sdr/FDEA202010012667.md): Panel · delaminated · Oct 1, 2020 · N562FE · Doug MD1010F · Wing, Plate/Skin
  > LT TRAILING EDGE TOP PANEL JUST ABOVE INBOARD FLAP OUTBOARD HINGE DELAMINATED REPAIRED PANEL ARC 0263-503, PER SRM 51-71-00 VOL 2 AND DWG ARC 0263.
- [SDR FDEA202010012486](https://openairdocs.org/sdr/FDEA202010012486.md): Stiffener · corroded · Oct 1, 2020 · N562FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > MAIN DECK LEFT SIDE AT APPROXIMATELY STA 1440 LONG 17, HAS EXFOLIATION CORROSION, MARKED NR 11. REQUIRES SDR. REMOVED AND REPLACED STIFFENER AEA0220-505, PER SRM 51-31-01 VOL II & 51-33-01 VOL II.
- [SDR FDEA202010012430](https://openairdocs.org/sdr/FDEA202010012430.md): Seat Track · damaged · Oct 1, 2020 · N562FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK LOBE WORN BEYOND LIMITS AT STA 985 LBL 12" REQUIRES R & R. REPLACED DAMAGED SEAT TRACK FROM STATION 969 TO STATION 989 LBL 12". REFERENCE SRM 53-70-00 FIG 1 VOL 1 SRM 51-31-01 VOL 2 FEDEX DWG SR10-53-002 AND SRM 51-41-01 VOL 2.
- [SDR FDEA202009302477](https://openairdocs.org/sdr/FDEA202009302477.md): Panel · corroded · Sep 30, 2020 · N562FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > LIGHT CORROSION UNDER NUTPLATE, RIGHT HAND SIDE FILET PANEL 152LT, MARKED WITH A TAG ON AIRCRAFT. REPAIRED PER SRM 53-00-01 FIG 7.
- [SDR FDEA202009292641](https://openairdocs.org/sdr/FDEA202009292641.md): Web · cracked · Sep 29, 2020 · N562FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > LT NLG WHEEL WELL WEB AT STA 495 HAS 2 EA CRACKS 4IN BELOW HORIZONTAL PRESSURE PANEL, MARKED. REPAIRED WHEEL WELL CRACKS AT STA 495, REF SRM 53-30-00 FIG 6 SH 2 VOL I. MAJOR REPAIR.
- [SDR FDEA202009292492](https://openairdocs.org/sdr/FDEA202009292492.md): Web · cracked · Sep 29, 2020 · N562FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > LT NLG WHEEL WELL WEB AT STA 495 HAS 2 EA, CRACKS 28 IN BELOW HORIZONTAL PRESSURE PANEL, MARKED. REPAIRED THE WEB LT SIDE AT STA 495, IN REF TO SRM 53-30-00 FIG 6 VOL 1.
- [SDR FDEA202009292462](https://openairdocs.org/sdr/FDEA202009292462.md): Web · cracked · Sep 29, 2020 · N562FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > RT NLG WHEEL WELL WEB AT STA 495 HAS 4 EA CRACKS 28 IN BELOW HORIZONTAL PRESSURE PANEL, MARKED. REMOVED DAMAGE AREA AND PERFORMED REPAIR ON RT NLG WHEEL WELL WEB AT STA 495, PER SRM 53-30-00 VOL 1 FIG 6 SHEETS 8-10.
- [SDR FDEA202009292392](https://openairdocs.org/sdr/FDEA202009292392.md): Floorboard · delaminated · Sep 29, 2020 · N562FE · Doug MD1010F · Fuselage Floor Panel
  > MAIN DECK FLOORBOARD HAS SMALL PUNCTURE, MARKED STA 1646 LBL 85. REPAIRED DAMAGE, REF SRM 53-60-00 FIG 6 PG 6 VOL I.
- [SDR FDEA202009292376](https://openairdocs.org/sdr/FDEA202009292376.md): Floorboard · dented · Sep 29, 2020 · N562FE · Doug MD1010F · Fuselage Floor Panel
  > MAIN DECK FLOORBOARD HAS SMALL INDENT IN SURFACE, MARKED STA 1105 LBL 85. REPAIRED INDENT IN SURFACE, PER SRM 53-60-00 VOL 1 FIG 7 PAGE 7.
- [SDR FDEA202009292375](https://openairdocs.org/sdr/FDEA202009292375.md): Floorboard · dented · Sep 29, 2020 · N562FE · Doug MD1010F · Fuselage Floor Panel
  > MAIN DECK FLOORBOARD HAS INDENT IN SURFACE, MARKED STA 1685 CENTERLINE. REPAIRED SMALL INDENT ON NOTED FLOORBOARD SURFACE, REF SRM 53-60-00 VOL 1 FIG 7 PG 7.
- [SDR FDEA202009292374](https://openairdocs.org/sdr/FDEA202009292374.md): Floorboard · dented · Sep 29, 2020 · N562FE · Doug MD1010F · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL HAS SMALL PUNCTURE, MARKED STA 1320 LBL 1. REPAIRED, PER SRM 53-60-00 VOL 1 FIG 7 PAGE 7.
- [SDR FDEA202009292373](https://openairdocs.org/sdr/FDEA202009292373.md): Floorboard · dented · Sep 29, 2020 · N562FE · Doug MD1010F · Fuselage Floor Panel
  > MAIN DECK FLOORBOARD HAS INDENT IN SURFACE, MARKED STA 1565 CENTERLINE. REPAIRED SMALL INDENT ON NOTED FLOORBOARD SURFACE, REF SRM 53-60-00 VOL1 FIG 7 PG 7.
- [SDR FDEA202009292372](https://openairdocs.org/sdr/FDEA202009292372.md): Floorboard · dented · Sep 29, 2020 · N562FE · Doug MD1010F · Fuselage Floor Panel
  > MAIN DECK FLOORBOARD HAS INDENT IN SURFACE, MARKED STA 1591 RBL 5. REPAIRED SMALL INDENT ON MAIN DECK FLOORBOARD SURFACE AT STA 1591 RBL 5, REF SRM 53-60-00 VOL 1 FIG 7 PG 7.
- [SDR FDEA202009292370](https://openairdocs.org/sdr/FDEA202009292370.md): Floorboard · dented · Sep 29, 2020 · N562FE · Doug MD1010F · Fuselage Floor Panel
  > MAIN DECK FLOORBOARD HAS INDENT IN SURFACE, MARKED STA 1631 LBL 7. REPAIRED PUNCTURE, PER SRM REF 53-60-00 FIG 7 PG7 VOL I.
- [SDR FDEA202009292369](https://openairdocs.org/sdr/FDEA202009292369.md): Floorboard · dented · Sep 29, 2020 · N562FE · Doug MD1010F · Fuselage Floor Panel
  > MAIN DECK FLOORBOARD HAS SMALL INDENT IN SURFACE, MARKED STA 1525 LBL 6. REPAIRED SMALL INDENT ON MAIN DECK FLOORBOARD SURFACE AT STA 1525 LBL 6, REF SRM 53-60-00 VOL 1 FIG 7 PG 7.
- [SDR FDEA202009292367](https://openairdocs.org/sdr/FDEA202009292367.md): Floorboard · delaminated · Sep 29, 2020 · N562FE · Doug MD1010F · Fuselage Floor Panel
  > MAIN DECK FLOORBOARD HAS INDENT IN SKIN, MARKED. STA 1510 AT CENTERLINE. REPAIRED DAMAGE, REF SRM 53-60-00 FIG 7 PG 7 VOL I.
- [SDR FDEA202009292366](https://openairdocs.org/sdr/FDEA202009292366.md): Floorboard · delaminated · Sep 29, 2020 · N562FE · Doug MD1010F · Fuselage Floor Panel
  > MAIN DECK FLOORBOARD HAS SMALL PUNCTURE, MARKED. STA 1441 CENTERLINE. REPAIRED DAMAGE, REF SRM 53-60-00 FIG 5 PG 5 VOL I.
- [SDR FDEA202007162371](https://openairdocs.org/sdr/FDEA202007162371.md): Floorboard · dented · Jul 16, 2020 · N562FE · Doug MD1010F · Fuselage Floor Panel
  > MAIN DECK FLOORBOARD HAS SMALL PUNCTURE, STA 1154 LBL8. REPAIRED PUNCTURE, PER SRM REF 53-60-00 FIG 7 PG7 VOL I.
- [SDR FDEA2020061671059](https://openairdocs.org/sdr/FDEA2020061671059.md): Indicator · failed · May 27, 2020 · N562FE · Doug MD1010F · Escape Slide
  > R1 SLIDE LIGHT IS INOP. REMOVED AND REPLACED R1 REMOTE SLIDE PACK PRESSURE INDICATOR REF AMM 25-61-03-2. R/R REMOTE SLIDE PACK PRESSURE INDICATOR PN 26C17528-2, NSN AND "C" CELL BATTERY P/N MN1400, NSN.
- [SDR FDEA2020052971059](https://openairdocs.org/sdr/FDEA2020052971059.md): Light · inoperative · May 27, 2020 · N562FE · Doug MD1010F · Emergency Lighting
  > R1 SLIDE LIGHT IS INOPERATIVE.
- [SDR FDEA201902260484](https://openairdocs.org/sdr/FDEA201902260484.md): Indication Sys · inoperative · Feb 12, 2019 · N562FE · Doug MD1010F · Escape Slide
  > R1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST INDICATION SYSTEM INOP ON PRE FLIGHT FACT 22FEB19 20:53 MEM U REMOVED AND REPLACED REMOTE SLIDE PACK PRESS INDICATOR. TEST GOOD. A/C OK FOR SERVICE. REF AMM 25-61-03-5/25-61-01-2.
- [SDR FDEA201901300230](https://openairdocs.org/sdr/FDEA201901300230.md): Light · false activation · Jan 30, 2019 · N562FE · Doug MD1010F · Door Warning System
  > L1 CABIN DOOR PRESS LIGHT ON CONTINUOUSLY CANNOT TEST. PERFORMED OPS CHECK OF L1 DOOR REMOTE PRESSURE LIGHT IAW AMM 25-61-03-5, OPS NORMAL.
- [SDR FDEA2018112103308](https://openairdocs.org/sdr/FDEA2018112103308.md): Indicator · damaged · Nov 20, 2018 · N562FE · Doug MD1010F · Emergency Equipment
  > DURING PREFLT CK FOUND L-1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO- TEST INDICATOR LIGHT ON. L-1 DOOR EVACUATION SLIDE PUSHBUTTON INDICATOR PLASTIC COVER FOUND BROKEN. REMOVED AND REPLACED L-1 DOOR EVACUATION SLIDE REMOTE PRESSURE PERSS-TO- TEST
- [SDR FDEA201811203311](https://openairdocs.org/sdr/FDEA201811203311.md): Indicator · inoperative · Nov 20, 2018 · N562FE · Doug MD1010F · Escape Slide
  > DURING PREFLT CK FOUND L1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATOR LIGHT ON. L-1 DOOR EVACUATION SLIDE PUSHBUTTON INDICATOR PLASTIC COVER FOUND BROKEN. REMOVED AND REPLACED L-1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST PUSHBUTT
- [SDR FDEA201811133196](https://openairdocs.org/sdr/FDEA201811133196.md): Switch · broken · Nov 13, 2018 · N562FE · Doug MD1010F · Emergency Equipment
  > PUSH TO TEST SWITCH FOR ESCAPE SLIDE ON L1 DOOR BROKEN. SECURED TEST SWITCH FOR L1 ESCAPE SLIDE. OPS VERIFED NORMAL
- [SDR FDEA201809252722](https://openairdocs.org/sdr/FDEA201809252722.md): Skin · cracked · Sep 25, 2018 · N562FE · Doug MD1010F · Trailing Edge Flaps
  > RT WING INBD FLAP UPPER SURFACE APPROX XIFH 207, TWO CRACKS AROUND FASTENERS. CONFIRMED USING NDT HFEC. DOUBLER REPAIRED PER SRM 57-10-00 FIG 85 SHEET 3 VOL 1. REF EA 8-5700-T0342609.
- [SDR FDEA201809252708](https://openairdocs.org/sdr/FDEA201809252708.md): Skin · corroded · Sep 25, 2018 · N562FE · Doug MD1010F · Wing, Plate/Skin
  > RH WING UPPER SURFACE CORROSION AROUND ONE FASTENER APPROX XORS 247 STRG 10. REMOVED CORROSION AROUND ONE FASTENER ON RH WING UPPER SURFACE AT APPROX 247 STRG 10 PER EA 8-5710-T0342473 P1.
- [SDR FDEA201809252707](https://openairdocs.org/sdr/FDEA201809252707.md): Skin · corroded · Sep 25, 2018 · N562FE · Doug MD1010F · Wing, Plate/Skin
  > RH WING UPPER SURFACE CORROSION AROUND THREE FASTENER APPX XORS 333 STRG 8. REMOVED CORROSION AROUND THREE FASTENERS XORS 333 STRG 8.
- [SDR FDEA201809172714](https://openairdocs.org/sdr/FDEA201809172714.md): Floor Support · corroded · Sep 17, 2018 · N562FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > AFT CARGO, CTR OF FLOOR SUPPORT (AGA3874-9) AT APPROX STA 1841 CORRODED ON L-ANGLE. REPAIRED CORRODED FLOOR SUPPORT, REF SRM 53-00-01 VOL I FIG 8, SHEET 2 AND DRAWING AGA3874 MAJOR REPAIR.
- [SDR FDEA201809052612](https://openairdocs.org/sdr/FDEA201809052612.md): Shear Tie · corroded · Sep 5, 2018 · N562FE · Doug MD1010F · Fuselage Internal Mounting Structure
  > AFT CARGO COMPT, APPROX STA 1885, LONG 43L. LONG SHEAR TIE END, IS CORRORED/CRACKED. INSTALLED AS REQ NEW LONG SHEAR TIE END AT STA 1885 L43 REF DWG NFA6074.
- [SDR FDEA201809032712](https://openairdocs.org/sdr/FDEA201809032712.md): Spar Cap · corroded · Sep 3, 2018 · N562FE · Doug MD1010F · Horizontal Stabilizer, Spar/Rib
  > LT HORIZONTAL STABILIZER XFS = 90 FRONT SPAR IB UPPER TEE CAP HAS 2" OF MINOR SURFACE CORROSION. MARKED REPAIRED UPPER FORWARD SPAR CAP ALC7082 REF SRM 55-20-00 FIG 9 SH 1 VOL I, MAJOR REPAIR.
- [SDR FDEA2018091812549](https://openairdocs.org/sdr/FDEA2018091812549.md): Seat Track · broken · Aug 31, 2018 · N562FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CARGO DECK APPROX STA 755 LBL 27.5 SEAT TRACK HAS BROKEN LOBE. REPLACED DAMAGED SEAT TRACK FROM STATION 715 TO STATION 772 LBL 27.5 REF SRM 53-70-00 FIG 1 VOL 1.
- [SDR FDEA201706201715](https://openairdocs.org/sdr/FDEA201706201715.md): Light · malfunctioned · Jun 20, 2017 · N562FE · Doug MD1010F · Emergency Equipment
  > R1 ENTRY DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATING SYSTEM DOES NOT ILLUMINATE. WHILE PERFORMING DAILY CHECK FOR R1 SLIDE BOTTLE PRESSURE, FOUND BOTTLE INDICATOR LIGHT WORKING NORMALLY. CHECKED CONDITION OF WIRING AND CONNECTIONS. NO D

Next page: https://openairdocs.org/deregistered/N562FE-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 = 'N562FE' AND deregistration_id = 'N562FE-2024-03-02'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N562FE-2024-03-02/reports

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