# Service difficulty reports: N374FE, cancelled Mar 22, 2017

A list on [N374FE, cancelled Mar 22, 2017](https://openairdocs.org/deregistered/N374FE-2017-03-22.md).

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

- [SDR 08FDEA00738](https://openairdocs.org/sdr/08FDEA00738.md): Reducer · leaking · Mar 5, 2008 · N374FE · Doug MD1010F · Hydraulic System, Main
  > HYD 3 ELEV OFF AND HYD 3 QTY LOW ALERT ANNUNCIATED. HYDRAULIC QUANTITY STABILIZED AT 3.9 GALLON. TIGHTENED "B" NUT UNION (REDUCER) ON RT MAIN LANDING GEAR SWIVEL GLAND, SERVICED HYDRAULICS'S AND LEAK CHECKED CHECKED GOOD IAW MD10-10 AMM 20-50-01-2 AND MD10-
- [SDR 08FDEA00522](https://openairdocs.org/sdr/08FDEA00522.md): Intercostal · corroded · Feb 20, 2008 · N374FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > LOWER AFT CARGO COMPARTMENT CORROSION ON INTERCOSTAL BETWEEN STRINGERS 44 AND 45 LT AT FS 1781. FABRICATED NEW INTERCOSTAL PER DAC DAW AFA 3870 REV F AND INSTALLED PER DC/MD10 SRM 51-33-01 VOL II.
- [SDR 08FDEA00515](https://openairdocs.org/sdr/08FDEA00515.md): Skin · corroded · Feb 19, 2008 · N374FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > CENTER WHEEL WELL LOWER SKIN HAS CORROSION FROM FS 1501 TO 1521 BETWEEN STR 50L TO51R. REMOVED, FABRICATED AND INSTALLED REPAIR PER E8-5330-113024" FUSELAGE-SKIN AT STA 1519 AND L-52-REPAIR.
- [SDR 08FDEA00450](https://openairdocs.org/sdr/08FDEA00450.md): Web · cracked · Feb 15, 2008 · N374FE · Doug MD1010F · Fuselage Miscellaneous Structure
  > CENTER CARGO COMP AT STA 1781 BELOW THE FLOOR AREA FROM L 52 - L 44 L WEB P/N AFA0154-5 1S CRACKED. FABRICATED NEW WEB PER REF. DAC DWG AFA 0154 REV. AT. INSTALLED IAW MD/DC 10 SRM 51-33-01 VOL. II. PART MARKED PER GMM7-0-1000. MINOR REPAIR.
- [SDR 08FDEA00449](https://openairdocs.org/sdr/08FDEA00449.md): Skin · corroded · Feb 15, 2008 · N374FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > CENTER WHEEL WELL LOWER INTERIOR SKIN HAS CORROSION BETWEEN STR 47 R AND STR 48 R FROM FS 1501 TO FS 1520. REMOVED, FABRICATED AND INSTALLED REPAIR PER E8-5330-113023 "FUSELAGE-SKIN AT STA 1507 AND 1519 AND L-48 RT-REPAIR.
- [SDR 08FDEA00451](https://openairdocs.org/sdr/08FDEA00451.md): Skin · corroded · Feb 15, 2008 · N374FE · Doug MD1010F · Wing, Plate/Skin
  > RIGHT WING UPPER TRAILING EDGE PANEL HAS CORROSION ON THE UPPER SURFACE, APPROXIMATELY XORS 345. REMOVED CORROSION; OUT OF LIMITS IAW 10 SRM 51-21-01, VOL II & 57-31-01 FIG A, VOL III & 57-00-01 FIG A, VOL I. REMOVED PANEL IAW SRM 51-33-01, VOL II, 51-3
- [SDR 08FDEA00339](https://openairdocs.org/sdr/08FDEA00339.md): Shear Tie · damaged · Jan 31, 2008 · N374FE · Doug MD1010F · Fuselage Internal Mounting Structure
  > FWD PIT AT STA 808 BETWEEN STR 42L AND STR 43L SHEARTIE HAS TOOL MARKS. FABBED NEW SHEARTIE IN REF TO FEDEX GMM 7-0-1001 AND DAC DWG RAM1470. REMOVED AND INSTALLED SHEARTIE AT STA 808 L42L - L43L IN REF TO DC/MD10-10 SRM 51-33-01 VOL II PG1.
- [SDR 08FDEA00328](https://openairdocs.org/sdr/08FDEA00328.md): Skin · misrepaired · Jan 30, 2008 · N374FE · Doug MD1010F · Trailing Edge Flaps
  > FOUND REPAIR DOUBLER R/W O/B FLAP LOWER SKIN STA XOF 458. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EVALUATED REPAIR AND FOUND NOT TO BE WITHIN THE LIMITS OF DC/MD10 SRM 57-10-00 FIG9 V
- [SDR 08FDEA00329](https://openairdocs.org/sdr/08FDEA00329.md): Skin · failed · Jan 30, 2008 · N374FE · Doug MD1010F · Trailing Edge Flaps
  > LT I/B FLAP LOWER EXTERNAL SURFACE HAS ERRODED DENT FILLER. REMOVED FILLER,FABRICATED AND INSTALLED NEW REPAIR IAW MD/DC10 SRM 57-10-00 FIG 85 VOLI, 51-21-01 VOLII.
- [SDR 08FDEA00315](https://openairdocs.org/sdr/08FDEA00315.md): Angle · corroded · Jan 28, 2008 · N374FE · Doug MD1010F · Fuselage Main, Bulkhead
  > LWW, SLANT BULKHEAD PANEL LWR ATTACH ANGLE CORRODED AT SEVERAL AREAS BET LT AND RT CORNERS, FWD AND AFT FACES, STA 1381. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW MD/DC 10SRM 53-00-01 FIG 1A VOL I. MACHINED NEW SETION DWG APB7080 REV. D. INSTALLED PER
- [SDR 08FDEA00313](https://openairdocs.org/sdr/08FDEA00313.md): Skin · corroded · Jan 28, 2008 · N374FE · Doug MD1010F · Fuel Storage
  > LWW, UPPER CTR TANK SKIN CORRODED, STA 1381, LBL 49. REMOVED AND REINSTALLED FASTENERS IAW SRM 51-31-01, VOL II. REMOVED CORROSION, FOUND TO BE WITHIN LIMITS IAW SRM 57-00-01 FIG 1A VOL I, AND SRM 53-33-01 FIG 1 VOL III. ALODINED AND PRIMED IAW SRM 51-21-0
- [SDR 08FDEA00311](https://openairdocs.org/sdr/08FDEA00311.md): Skin · corroded · Jan 28, 2008 · N374FE · Doug MD1010F · Fuel Storage
  > LWW, CTR TANK UPPER SKIN CORRODED STA 1381, LBL 76. REMOVED AND REINSTALLED FASTENERS IAW 51-31-01 VOL II. REMOVED CORROSION, FOUND TO BE WITHIN LIMITS IAW SRM 57-00-01 FIG 1A VOL I AND SRM 57-33-01 FIG 1 VOL III. ALODINED AND PRIMED IAW SRM 51-21-01 VOL II
- [SDR 08FDEA00281](https://openairdocs.org/sdr/08FDEA00281.md): Floorbeam · corroded · Jan 25, 2008 · N374FE · Doug MD1010F · Fuselage Main, Floor Beam
  > FWD PIT AT STA 879 RBL 57 FLOORBEAM HAS CORROSION. FOUND TO BE OUT OF LIMITS AND REPAIRED BY SPLICING IN NEW SECTION OF FLOORBEAM IAW SRM 53-00-01 VOL I FIG 7. THIS REPAIR IS CLASSIFIED AS MAJOR. ROLLER TRAY AT STA 765-879 RBL 56 REMOVED FOR ACCESS AND REIN
- [SDR 08FDEA00280](https://openairdocs.org/sdr/08FDEA00280.md): Frame · corroded · Jan 25, 2008 · N374FE · Doug MD1010F · Fuselage Main, Frame
  > FWD PIT AT STA 919 BETWEEN STR 51R AND 51L LOWER FLANGE, FRAME HAS CORROSION. REPAIRED LOWER FLANGE AT STA 919, LONG 51R & 51L IAW DC/MD10-10 SRM 53-30-00, VOL I FIGURE 5
- [SDR 08FDEA00282](https://openairdocs.org/sdr/08FDEA00282.md): Door Frame · cracked · Jan 25, 2008 · N374FE · Doug MD1010F · Fuselage Main, Structure
  > NR 3 MCD LOWER JAMB SUPPORT FITTING HOLES A, B, C AND D HAS CRACK INDICATIONS FOUND WITH BHE (SEE ATTACHED DRAWING). INSTALLED REPAIR BUSHINGS IN REFERENCE WITH DC/MD10-10 SRM VOLUME I, 53-50-00 PAGE 81 FIGURE 17 AT HOLE LOCATIONS A, B, C AND D TO CARGO DOOR
- [SDR 08FDEA00286](https://openairdocs.org/sdr/08FDEA00286.md): Door Frame · cracked · Jan 25, 2008 · N374FE · Doug MD1010F · Fuselage Main, Structure
  > NR 6 MCD LOWER JAMB SUPPORT FITTING HOLES A, C AND D HAS CRACK INDICATIONS FOUND WITH BHEC (SEE ATTACHED DRAWING). INSTALLED REPAIR BUSHINGS IN REFERENCE WITH DC/MD10-10 SRM VOLUME I, 53-50-00, PAGE 81 FIG 17 AT HOLE LOCATIONS A, C, AND D TO CARGO DOOR JAMB
- [SDR 08FDEA00285](https://openairdocs.org/sdr/08FDEA00285.md): Door Frame · cracked · Jan 25, 2008 · N374FE · Doug MD1010F · Fuselage Main, Structure
  > NR 6 MCD LOWER JAMB SUPPORT FITTING HOLES A, C AND D HAS CRACK INDICATIONS FOUND WITH BHEC (SEE ATTACHED DRAWING). INSTALLED REPAIR BUSHINGS IN REFERENCE WITH DC/MD10-10 SRM VOLUME I, 53-50-00, PAGE 81 FIG 17 AT HOLE LOCATIONS A, C, AND D TO CARGO DOOR JAMB
- [SDR 08FDEA00284](https://openairdocs.org/sdr/08FDEA00284.md): Door Frame · cracked · Jan 25, 2008 · N374FE · Doug MD1010F · Fuselage Main, Structure
  > NR 4 MCD LOWER JAMB SUPPORT FITTING HOLES A, B, C AND D HAS CRACK INDICATIONS FOUND WITH BHEC (SEE ATTACHED DRAWING). INSTALLED REPAIR BUSHINGS IN REFERENCE WITH DC/MD10-10 SRM VOLUME I, 53-50-00 PAGE 81 FIG 17 AT HOLE LOCATIONS A, B, C AND D TO CARGO DOOR JA
- [SDR 08FDEA00283](https://openairdocs.org/sdr/08FDEA00283.md): Door Frame · cracked · Jan 25, 2008 · N374FE · Doug MD1010F · Fuselage Main, Structure
  > NR 1 MCD LOWER JAMB SUPPORT FITTING HOLE "C" HAS CRACK INDICATIONS, FOUND WITH BHEC (SEE ATTACHED DRAWING). INSTALLED REPAIR BUSHING IN REFERENCE WITH DC/MD10-10 SRM VOLUME I 53-50-00 PAGE 81 FIG 17 AT HOLE LOCATION C, TO CARGO DOOR JAMB BEAM ONLY. LOWER FIT
- [SDR 08FDEA00276](https://openairdocs.org/sdr/08FDEA00276.md): Shear Tie · damaged · Jan 25, 2008 · N374FE · Doug MD1010F · Fuselage Internal Mounting Structure
  > FWD PIT AT STA.808 BETWEEN STRINGER 34R AND 35R SHEAR TIE DAMAGED ON RADIUS. REMOVED, FABRICATED AND INSTALLED SHEAR TIE PER DC/MD10-10 SRM 53-13-01 VOL III FIG 8A AND 53-30-00 VOL I FIG10 AND 53-30-00 VOL I PAGE 34 FIG 9.
- [SDR 08FDEA00245](https://openairdocs.org/sdr/08FDEA00245.md): Shear Tie · corroded · Jan 23, 2008 · N374FE · Doug MD1010F · Fuselage Internal Mounting Structure
  > LOWER FORWARD CARGO, STA 1099 BETWEEN L33L AND L35L, SHEAR TIE HAS CORROSION ON LOWER FLANGE, PART ADA0003-19 REMOVED CORROSION IAW DC/MD10-10 SRM, VOLUME II, 51-21-01 PAGE 28. ORIGINAL THICKNESS IS.071 IAW DAC DWG ADA0003, REV M, PARTS LIST, ITEM -19. MATE
- [SDR 08FDEA00222](https://openairdocs.org/sdr/08FDEA00222.md): Frame · corroded · Jan 22, 2008 · N374FE · Doug MD1010F · Fuselage Main, Frame
  > FOUND CORROSION ON FRAME LOWER SURFACE, FS 1099 BETWEEN L34L AND L35L. REMOVED CORROSION IAW SRM VOL II 51-21-01 PG 28A. FOUND TO BE OUT OF LIMITS IAW SRM VOL I 53-00-01 FIG 5 SHT 1. REMOVED AND REINSTALLED STRAP AND ANGLE IAW SRM VOLII 51-33-01. REMOVED
- [SDR 08FDEA00210](https://openairdocs.org/sdr/08FDEA00210.md): Shear Tie · corroded · Jan 21, 2008 · N374FE · Doug MD1010F · Fuselage Internal Mounting Structure
  > CAC, CORROSION, SHEAR TIE, FS 1099 BETWEEN L51 R AND L50R REMOVED CORROSION IN REFERENCE WITH DC/MD10-10 SRM, VOLUME II, 51-21-01, PAGE 28A. ORIGINAL THICKNESS IA.071 INCH IAW DC/MD10-10 SRM, VOL III 53-13-01, FIGURE 8A, SHEET 1, ITEM 33. MATERIAL REMOVED
- [SDR 08FDEA00203](https://openairdocs.org/sdr/08FDEA00203.md): Seat Track · gouged · Jan 18, 2008 · N374FE · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > MCD STA 1239 RBL 48 SEAT TRACK GOUGED AND WORN EVALUATED SEAT TRACK; SEVERAL BROKEN SCALLOPS, OUT OF LIMITS IAW DC/MD10-10 SRM 53-70-00 VOL I PG 21. REMOVED AND REINSTALLED 4 FLOOR PANELS AT STA 1199-1321 AND 1199-1259 RBL 27-76 IAW MD/DC 10-10 M/M 53-21-01-2
- [SDR 08FDEA00201](https://openairdocs.org/sdr/08FDEA00201.md): Shear Tie · damaged · Jan 18, 2008 · N374FE · Doug MD1010F · Fuselage Internal Mounting Structure
  > FWD PIT AT STA 808 BETWEEN LONG 34R AND LONG 35R SHEAR TIE DAMAGED ON RADIUS. REMOVED, FABRICATED, AND INSTALLED SHER TIE PER SRM 53-13-01, VOL III FIG 8A AND SRM 53-30-00 VOL I FIG 10 AND SRM 53-30-00 VOL I PAGE 34 FIG 9 MAJOR REPAIR.
- [SDR 08FDEA00200](https://openairdocs.org/sdr/08FDEA00200.md): Shear Tie · corroded · Jan 18, 2008 · N374FE · Doug MD1010F · Fuselage Internal Mounting Structure
  > LOWER FORWARD CARGO, STA 1099 BETWEEN L33L AND L35, SHEAR TIE HAS CORROSION ON LOWER FLANGE. REMOVED CORROSION IAW SRM VOLUME II, 51-21-01 PAGE 28. FOUND TO BE OUT OF LIMITS IAW SRM, VOLUME I, 53-00-01, FIGURE 1B. FABRICATED NEW -19 IAW DAC DGW ADA0003
- [SDR 08FDEA00198](https://openairdocs.org/sdr/08FDEA00198.md): Support Fitting · cracked · Jan 18, 2008 · N374FE · Doug MD1010F · Fuselage Main, Structure
  > NR 2 MCD LOWER JAMB SUPPORT FITTING HOLES A, B AND C HAS CRACK INDICATIONS, FOUND WITH BHEC. INSTALLED REPAIR BUSHINGS AT LOCATION NR 2 FITTING HOLES A, B AND C IAW SRM 53-50-00 VOL I PG 81 FIG 17.
- [SDR 08FDEA00195](https://openairdocs.org/sdr/08FDEA00195.md): Support Fitting · cracked · Jan 18, 2008 · N374FE · Doug MD1010F · Fuselage Main, Structure
  > NR 5 MCD LOWER JAMB SUPPORT FITTING HOLES A AND D HAS CRACK INDICATIONS FOUND WITH BHEC. INSTALLED REPAIR BUSHINGS IAW SRM 53-50-00 VOL I PG 81 FIG 17 AT NR 5 FITTING LOCATION
- [SDR 08FDEA00159](https://openairdocs.org/sdr/08FDEA00159.md): Fitting · cracked · Jan 15, 2008 · N374FE · Doug MD1010F · Cargo/Baggage Doors
  > UPPER MAIN CARGO DOOR, LOWER JAMB SUPPORT FITTING NR 7 IS CRACKED IN HOLES "A, B, D" BEYOND SRM LIMITS. REPLACED SUPPORT FITTING NR 7 MAIN CARGO DOOR SPOOL LOCATION IAW SRM 51-33-01 VOL II.
- [SDR 08FDEA00158](https://openairdocs.org/sdr/08FDEA00158.md): Fitting · cracked · Jan 15, 2008 · N374FE · Doug MD1010F · Cargo/Baggage Doors
  > UPPER MAIN CARGO DOOR, LOWER JAMB SUPPORT FITTING NR 6 IS CRACKED IN HOLE "A" BEYOND SRM LIMITS. REPLACED SUPPORT FITTING NUMBER 6 MAIN CARGO DOOR SPOOL LOCATION IN REF TO SRM 51-33-01 VOL II P/N AFA7132-1.
- [SDR 08FDEA00157](https://openairdocs.org/sdr/08FDEA00157.md): Support Fitting · cracked · Jan 15, 2008 · N374FE · Doug MD1010F · Cargo/Baggage Doors
  > UPPER MAIN CARGO DOOR, LOWER JAMB SUPPORT FITTING NR 4 IS CRACKED IN HOLES "A, C, D" BEYOND SRM LIMITS. REPLACED SUPPORT FITTING NR 4 MAIN CARGO DOOR SPOOL LOCATION IAW SRM 51-33-01 VOL II.
- [SDR 08FDEA00156](https://openairdocs.org/sdr/08FDEA00156.md): Support Fitting · cracked · Jan 15, 2008 · N374FE · Doug MD1010F · Cargo/Baggage Doors
  > UPPER MAIN CARGO DOOR, LOWER JAMB SUPPORT FITTING NR 3 IS CRACKED IN HOLE "B" BEYOND SRM LIMITS. REPLACED SUPPORT FITTING NUMBER 3 MAIN CARGO DOOR SPOOL LOCATION IAW SRM 51-33-01 VOL II.
- [SDR 08FDEA00155](https://openairdocs.org/sdr/08FDEA00155.md): Support Fitting · cracked · Jan 15, 2008 · N374FE · Doug MD1010F · Cargo/Baggage Doors
  > UPPER MAIN CARGO DOOR, LOWER JAMB SUPPORT FITTING NR 1 IS CRACKED IN HOLE "C" BEYOND SRM LIMITS. REPLACED SUPPORT FITTING NR 1 MAIN CARGO DOOR SPOOL LOCATION IAW SRM 51-33-01 VOL II.
- [SDR 08FDEA00122](https://openairdocs.org/sdr/08FDEA00122.md): Skin · cracked · Jan 14, 2008 · N374FE · Doug MD1010F · Horizontal Stabilizer, Plate/Skin
  > 1 5/8" CRACK LOCATED ON THE RT HORIZONTAL STABILIZER AT THE INBOARD AFT CORNER OF THE OUTER SECTION UPPER AFT SKIN PANEL. END OF CRACK MARKED AND VERIFIED WITH HFEC INSPECTION. REPAIRED SKIN PLANK IAW EA 8-5510-116939, MAJOR REPAIR.
- [SDR 08FDEA00121](https://openairdocs.org/sdr/08FDEA00121.md): Skin · cracked · Jan 14, 2008 · N374FE · Doug MD1010F · Horizontal Stabilizer, Plate/Skin
  > LT HORIZONTAL STAB UPPER REAR SKIN PANEL CRACKED, INITIATING FROM AFT EDGE OF SKIN AND PROCEDING FWD 21/4" (APPROXIMATELY). VERIFIED BY HFEC INSPECTION MARKED END OF CRACK. COMPLIED WITH AE 8-5510-116939. MAJOR REPAIR.
- [SDR 06FDEA3066](https://openairdocs.org/sdr/06FDEA3066.md): Pressure Switch · failed · Aug 23, 2006 · N374FE · Doug MD1010F · Pneumatic Indicating System
  > NR 3 MANF FAIL INFLIGHT WHEN WING ANTI ICE SELECTED. FL340. COMPLIED WITH QRH. PERFORMED DECAY CHECK ON THE NR 3 MANIFOLD IAW MM 36-00-01-5, SYSTEM PASSED. CHECKED MANIFOLD FAIL DETECT UNIT IN CAC. FOUND RT WING PRESSURE SWITCH FAULTED. REMOVED AND REPLA
- [SDR 05FDEA00106](https://openairdocs.org/sdr/05FDEA00106.md): Valve · malfunctioned · Jan 17, 2005 · N374FE · Doug MD1010F · Air Intake Anti/De-Ice System
  > ENG 3 A-ICE DISAGREEMENT, LEVEL ONE ALERT ILLUMINATED STEADY WITH SWITCH IN EITHER POSITION. ENG NR 3 ANTI-ICE VALVE - INOP, FOUND OLD VALVE WAS BINDING SEVERLY AND DISAGREE LIGHT SWITCH WAS INOP ON VALVE. REMOVED AND REPLACED NR 3 NOSE COWL ANTI-ICE VALVE.
- [SDR 05FDEA00043](https://openairdocs.org/sdr/05FDEA00043.md): Skin · damaged · Aug 14, 2004 · N374FE · Doug MD1010F · Fuselage Main, Plate/Skin
  > NOT APPROVED FUSELAGE SKIN REPAIR AT LT AND RT LONG 44-47, STA 1526. SUBJECT REPAIRS WERE INSPECTED FOR COMPLIANCE WITH 14CFR 121.368, THE REPAIRS WERE EVALUATED TO BE ACCEPTABLE AS PERMANENT, PROVIDED REPAIRS ARE MODIFIED BY FEDEX EA 8-5310-84848.
- [SDR 05FDEA00044](https://openairdocs.org/sdr/05FDEA00044.md): Rail · corroded · Jun 10, 2004 · N374FE · Doug MD1010F · Fuselage Main, Structure
  > BULK CARGO DOOR JAMB RAIL P/N AFA3249-1 CORRODED APPROX AT STA 1755-1764. FILLER, CAP AND REPAIR ANGLE INSTALLED AFTER CORROSION REMOVAL IAW FEDEX EA 8-5310- 79980.
- [SDR 04FDEA00226](https://openairdocs.org/sdr/04FDEA00226.md): Proximity Switch · faulty · Jan 26, 2004 · N374FE · Doug DC1010 · Landing Gear Position and Warning
  > WHEN WE LOWERED THE GEAR FOR LANDING WE FELT THE GEAR COME DOWN BUT RED LIGHTS STAYED ON. WE MOVED THE HANDLE A FEW TIMES BUT NO HELP. RECYCLED GEAR AND THE RED LIGHTS STAYED ON. JIGGLED THE HANDLE AND THE LIGHTS FINALLY TURNED GREEN ALL AT THE SAME TIME.
- [SDR 03FDEA01681](https://openairdocs.org/sdr/03FDEA01681.md): Switch · inoperative · Oct 2, 2003 · N374FE · Doug DC1010 · Door Warning System
  > AIR CONDITIONING DOORS LIGHT ON S/O PANEL BEGAN FLICKERING INFLIGHT. FUEL WAS DUMPED AND LANDING ACCOMPLISHED AT SLC IAW RED TABS. ACN RELEASED FOR SERVICE IAW MEL/CDL: 52-04-04 CATEGORY: C EXPIRATION: 11OCT03, FACT 03OCT03 07:58 EWR R. REMOVED AND REPLA
- [SDR 2000ZZZX654](https://openairdocs.org/sdr/2000ZZZX654.md): Web · cracked · Feb 11, 2000 · N374FE · Doug DC1010 · Fuselage Miscellaneous Structure
  > DURING MAINTENANCE, THREE 10 INCH CRACKS WERE FOUND ON RIGHT/CENTER WHEELWELL (Y=1386, Z=52) COMMON TO KEEL WEB, WEB DOUBLER, AND UPER WEB SPLICE, P/N'S, AEA0161-3, AEA0161-153, AND AEA0501 RESPECTIVELY. DATA WAS SENT TO BOEING/DOUGLAS 5-14-99 AND RESENT 7-9
- [SDR 99FDEA00269](https://openairdocs.org/sdr/99FDEA00269.md): Web · cracked · May 3, 1999 · N374FE · Doug DC1010 · Fuselage Main, Keel
  > DUR A/C P-F CONV AT AERONAVALI, 3 10' CRACKS WERE FOUND AT Y=1386 COMMON TO KEEL WEB, WEB DOUBLER & AEA0501 KEEL WEB UPPER SPLICE. REPAIRED KEEL WEB AND WEB DOUBLER PER IAW FEDEX EA NR 8-5314-44061.
- [SDR 99FDEA00270](https://openairdocs.org/sdr/99FDEA00270.md): Skin · cracked · Nov 27, 1998 · N374FE · Doug DC1010 · Wing, Plate/Skin
  > DUR A/C P-F CONV FOUND DAMAGE AT XIFH=288.14 ON THE UPPER SURFACE OF LT I/B FLAP SKIN. REMOVED AND REPLACED O/B UPPER SKIN SECTION DAMAGE ARC2369. SRM 57-10-00 FIG 4 IAW FEDEX IAW EA NR 8-5752-44069.
- [SDR 99FDEA00271](https://openairdocs.org/sdr/99FDEA00271.md): Bolt · corroded · Oct 26, 1998 · N374FE · Doug DC1010 · Fuselage, Equipment Attach Fittings
  > DUR A/C P-F CONV CORROSION WAS FOUND IN ALL FOUR HOLE BORES COMMON TO ABA7003-2 & ABA7172 FITTINGS. THREE BOLTS FAILED IN TENSION. REMOVED AND REPLACED BOLTS FROM BORES IAW FEDEX EA NR 8-5311-41885.
- [SDR 99FDEA00272](https://openairdocs.org/sdr/99FDEA00272.md): Skin · corroded · Oct 2, 1998 · N374FE · Doug DC1010 · Fuselage Main, Plate/Skin
  > DUR A/C P-F CONV ON EXT LWR FUSELAGE FROM BS 1099 TO BS 1541 CORROSION. REMOVED AND REPLACED FUSELAGE BELLY SKIN FROM Y=1119 TO Y-1308, BETWEEN L48L-L48R. REPAIRED THEN INSTALLED AN EXT SKIN SPLICE SIMILAR TO SRM 5320, FIG 17 AT Y-1308 TO RESTORE STRENGTH IA

## 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 = 'N374FE' AND deregistration_id = 'N374FE-2017-03-22'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N374FE-2017-03-22/reports

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