# Service difficulty reports: N144FE, cancelled Aug 26, 2004

A list on [N144FE, cancelled Aug 26, 2004](https://openairdocs.org/deregistered/N144FE-2004-08-26.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 · 61 reports

- [SDR 02FDEA00315](https://openairdocs.org/sdr/02FDEA00315.md): Wire · damaged · May 7, 2002 · N144FE · Boeing 72721C · Flight Control System Wiring
  > DURING TAXI ELEVATOR FEEL DIFFERENTIAL LIGHT CAME ON. LOW PRESS LIGHT C/B ON. HYD A & B FILTERS CHECK GOOD. PITOT TUBES ON TAIL WERE CLEAN. SPLICED IN NEW SECTION OF WIRE PER SMP, OPS CHECK NORMAL.
- [SDR 00FDEA00391](https://openairdocs.org/sdr/00FDEA00391.md): Door · not closed · Jun 16, 2000 · N144FE · Boeing 72721C · Service Doors
  > AIRFRAME VIBRATION AND HUMMING SOUND. INSP GROUND PWR SERVICE DOOR. NO DEFECTS NOTED. RESECURED DOOR CLOSED.
- [SDR 00FDEA00273](https://openairdocs.org/sdr/00FDEA00273.md): Handle · worn · Apr 19, 2000 · N144FE · Boeing 72721C · Landing Gear Selector
  > ON FINAL APPROACH, GEAR HANDLE DOWN, HEARD NOISE. FELT MUSHY. NOSE GEAR AND NOSE DOORS UNSAFE RED LIGHT ON RECYCLED GOT GOOD IND ON ALL 3 GEAR. LANDING GEAR CONTROL HANDLE CABLE TENSION LOW. ADJUSTED PER MM 32-31-000-5 PG 501-505. REMOVED AND REPLACED SEL
- [SDR 99FDEA00268](https://openairdocs.org/sdr/99FDEA00268.md): Warning Switch · inop · Jul 21, 1999 · N144FE · Boeing 72721C · Landing Gear Position and Warning
  > ON DEPART, RT MLG DOOR APPEAR TO REMAIN OPEN EVEN AFTER CYCLING MLG PER RED TAB PROC. REMOVED AND REPLACED RT GEAR DOOR WARN SWITCH PER MM 32-62-011-4 ADJ & TEST PER MM 32-62-011-5. OPS CK GOOD.
- [SDR 99FDEA00179](https://openairdocs.org/sdr/99FDEA00179.md): Hose · leaks · May 14, 1999 · N144FE · Boeing 72721C · Overheat Detection
  > 99-113 - LWR AFT BODY O/H LIGHT ILLUM. LIGHT WENT OUT AFTER CLOSE NR 1 BLD AND BEFORE TURN OFF NR 1 PACK. 3RD TIME WRITTEN UP. REMOVED AND REPLACED SENSE LINE. OPER AND LEAK CK NORM.
- [SDR 99FDEA00178](https://openairdocs.org/sdr/99FDEA00178.md): Overheat Loop · inoperative · May 13, 1999 · N144FE · Boeing 72721C · Overheat Detection
  > 99-112 - LWR AFT BODY LIGHT ILLUM. LIGHT EXTINGUISH WHEN RT PACK AND RT BLD TURN OFF. REMOVED AND REPLACED LOOP PER MM 26-14-001-4. OPER CK NORM.
- [SDR 99FDEA00175](https://openairdocs.org/sdr/99FDEA00175.md): Overheat Light · malfunctioned · May 12, 1999 · N144FE · Boeing 72721C · Overheat Detection
  > LOWER AFT BODY O/H LIGHT ON. LIGHT WENT OUT WHEN NR 1 BLD AND LT PACK TURN OFF. INSP DUCT IN AFT AIR STAIRS, CEILING, KEEL BEAM AREA AND NO LEAKS FOUND. COULD NOT DUP O/H COND. OK TO CONTINUE SERVICE.
- [SDR 99FDEA00005](https://openairdocs.org/sdr/99FDEA00005.md): Valve · failed · Jan 6, 1999 · N144FE · Boeing 72721C · Pneumatic Distribution System
  > LOWER AFT BODY O/H LIGHT ILLUMINATED. FOLLOWED CK LIST PROCEDURE, CLOSED NR 1 BLEED VALVE AND LEFT PACK. RETARDED NR 1 THROTTLE TO CLIMB POWER. LIGHT REMAINED OUT AND TEST OK, INDICATIVE OF LEAK BETWEEN NR 1 BLEED VALVE AND LEFT PACK VALVE. REMOVED AND REP
- [SDR 98FDEA00487](https://openairdocs.org/sdr/98FDEA00487.md): Bear Strap · corroded · Aug 3, 1998 · N144FE · Boeing 72721C · Fuselage Main, Plate/Skin
  > STA-PAE: CORROSION (C53-224-02) INNER SKIN EMANATING FROM UNDER BEAR STRAP AT BS 475 BETWEEN STRINGER 3 AND 4 LT.
- [SDR 98FDEA00479](https://openairdocs.org/sdr/98FDEA00479.md): Spar Chord · corroded · Jul 30, 1998 · N144FE · Boeing 72721C · Wing Spar
  > CORROSION (C53-132-01-1) ON WING CENTER SECTION SPAR CHORD (LOWER) AT BS 745, RBL 12 TO RBL 30, WL 160. *S/D* REMOVED AND REPLACED LOWER SPAR CHORD, BS 745 IAW FED-EX DRAWING 65C21537.
- [SDR 98FDEA00477](https://openairdocs.org/sdr/98FDEA00477.md): Spar Chord · corroded · Jul 28, 1998 · N144FE · Boeing 72721C · Wing Spar
  > CORROSION (C57-562-02) RT WING SPAR LOWER CHORD HORIZONTAL LEG FS 456 TO 457. *S/D* REPAIRED RT WING FRONT SPAR LOWER SPAR CHORD AT FS 456 TO 467 IAW FED-EX EA 7-5710-35089.
- [SDR 98FDEA00471](https://openairdocs.org/sdr/98FDEA00471.md): Web · corroded · Jul 23, 1998 · N144FE · Boeing 72721C · Fuselage Miscellaneous Structure
  > WHILE WORKING NR 0840, FOUND CORROSION ON SHEAR WEB BS 1136, RBL 26 TO RBL 44, WL 208 ON UNDER SURFACE OF WEB. *S/D* REPAIRED SHEAR WEB BS 1136, RBL 26 TO RBL 44, WL 208 IAW FED-EX SRM 51-40-2.
- [SDR 98FDEA00465](https://openairdocs.org/sdr/98FDEA00465.md): Floorbeam · corroded · Jul 23, 1998 · N144FE · Boeing 72721C · Fuselage Main, Floor Beam
  > CORROSION (C53-224-06) IN SEVERAL AREAS ON THE UPPER CHORD OF THE BS 344 FLOORBEAM FROM LBL 63 TO RBL 21. REMOVED, FABRICATED AND INSTALLED FLOORBEAM UPPER CHORD AT BS 344, LBL 65 TO RBL 65 IAW FEDEX SRDM 27-53-007.
- [SDR 98FDEA00462](https://openairdocs.org/sdr/98FDEA00462.md): Stringer · corroded · Jul 17, 1998 · N144FE · Boeing 72721C · Fuselage Main, Longeron/Stringer
  > CORROSION (C53-224-02) ON STRINGER 9 LT, BS 380 TO 460. *S/D* REPAIRED STR 9 LT, BS 380 TO 480 PER FED-EX SRM 53-10-3.
- [SDR 98FDEA00461](https://openairdocs.org/sdr/98FDEA00461.md): Stringer · corroded · Jul 17, 1998 · N144FE · Boeing 72721C · Fuselage Main, Longeron/Stringer
  > CORROSION (C53-224-02) ON STRINGER 1 BL 0 BS 560 TO 580, BS 520 TO 540. *S/D* REMOVED CORROSION FROM STR 1, FOUND IT TO BE OUT OF LIMITS. REPAIRED STR 1, BS 520 TO 540 IAW FED-EX SRM 53-10-3.
- [SDR 98FDEA00366](https://openairdocs.org/sdr/98FDEA00366.md): Stringer · corroded · May 27, 1998 · N144FE · Boeing 72721C · Fuselage Main, Longeron/Stringer
  > NR 0684 044, CORROSION (C53-224-01(3)) ON STRINGER 2 LT, BS 950-1050. REPAIRED NR 2 LT STRINGER, BS 950-1050 IAW FED-EX SRM 53-10-3.
- [SDR 98FDEA00121](https://openairdocs.org/sdr/98FDEA00121.md): Frame · cracked · Feb 20, 1998 · N144FE · Boeing 72721C · Fuselage Main, Frame
  > NR 0926 043, STA-PAE - WHILE WORKING NR 0920 FOUND FRAME BEHIND NR 3 WINDOW ON THE RT SIDE AT BS 254, STR 9-11 RT TO BE CRACKED. REMOVED FRAME RT SIDE AT BS 254, STR 9-11. FABRICATED FRAME FROM 7075-T6.040. ALODINED AND PRIMED. INSTALLED FRAME IAW SRM 51-1
- [SDR 98FDEA00109](https://openairdocs.org/sdr/98FDEA00109.md): Skin · cracked · Feb 16, 1998 · N144FE · Boeing 72721C · Fuselage Main, Plate/Skin
  > NR 0920 042, WHILE PERFORMING HFEC INSPECTION OF FASTENER HOLES. FOUND CRACK EMANATING FROM HOLE AT BS 259.5, STR 8 R. REPAIRED CRACK AT BS 259.5, STR 8R PER EO 7-5330-7-2319G PT5 AND DRAWING 69-62161.
- [SDR 98FDEA00095](https://openairdocs.org/sdr/98FDEA00095.md): Long Beam · corroded · Feb 10, 1998 · N144FE · Boeing 72721C · Fuselage Main, Longeron/Stringer
  > NR 0557 041 STA-PAE - CORROSION (C53-224-01(2)) AROUND NUTCLIP HOLES LBL 45 LONGITUDINAL BEAM BS 838-843, WL 208. REMOVED AND REPLACED LBL 45 LONGITUDINAL BEAM WL 208 FROM BS 740 TO BS 848.5 PER BOEING 727 DRAWING 65-34144.
- [SDR 97FDEA00874](https://openairdocs.org/sdr/97FDEA00874.md): Bottle Fitting · corroded · Dec 3, 1997 · N144FE · Boeing 72721C · Fuselage, Wing Attach Fittings
  > WHILE WORKING NR0748, DISCOVERED CORROSION ON AFT SIDE OF RT BOTTLE FITTING, BS 870, RBL 66, WL 184. *S/D* REMOVED CORROSION, BLENDED ON AFT SIDE OF RT BOTTLE PIN COATING, FOUND COATING TO BE IN LIMITS PER FED EA 7-5710-35103.
- [SDR 97FDEA00809](https://openairdocs.org/sdr/97FDEA00809.md): Switches · moisture contam · Nov 7, 1997 · N144FE · Boeing 72724C · Landing Gear Position and Warning
  > RIGHT MAIN GEAR DOOR LIGHT ON SECOND OFFICER'S ANNUNCIATOR PANEL AND RED GEAR DOOR LIGHT ON GEAR POSITION PANEL REMAINED ILLUMINATED AFTER EXTENSION. GEAR INDICATION NORMAL AFTER RECYCLING. INSPECTED DOOR SWITCHES, FOUND SOME MOISTURE, CLEANED WITH CONTACT C
- [SDR 97FDEA00724](https://openairdocs.org/sdr/97FDEA00724.md): Skin · corroded · Oct 10, 1997 · N144FE · Boeing 72721C · Fuselage Main, Plate/Skin
  > BULGE IN SKIN LAP AT STR 20, BS 1070 LEFT HAND SIDE. *S/D* REMOVED CORROSION AND REPAIRED SKIN LAP AT STR 20 LEFT HAND BS 1070 PER FED-EX SRM 53-30-3 FIG 14.
- [SDR 97FDEA00717](https://openairdocs.org/sdr/97FDEA00717.md): Floorbeam · corroded · Oct 9, 1997 · N144FE · Boeing 72721C · Fuselage Main, Floor Beam
  > CORROSION ON UPPER CHORD OF FLOORBEAM AT BS 312, LBL 30, WL 208. *S/D* FOUND CORROSION TO BE OUT OF LIMITS. REMOVED CORROSION AT BS 312 FLOORBEAM UPPER CHORD LBL 30, WL 208 IAW FED-EX SRM 53-10-8 FED-EX SRM 53-10-1.
- [SDR 97FDEA00704](https://openairdocs.org/sdr/97FDEA00704.md): Skin · corroded · Oct 6, 1997 · N144FE · Boeing 72721C · Fuselage Main, Plate/Skin
  > WHILE WORKING NR0768, DISCOVERED CORROSION ON UPPER SKIN IN NR 2 TANK FROM BS 867 TO BS 870, RBL 65 TO LBL 65, WL 190. *S/D* REMOVED CORROSION ON LOWER SURFACE OF UPPER SKIN IN NR 2 TANK FROM BS 867 TO BS 870, RBL 65 TO LBL 65, WL 190 AND REPAIRED PER FED-EX
- [SDR 97FDEA00697](https://openairdocs.org/sdr/97FDEA00697.md): Chord · cracked · Oct 1, 1997 · N144FE · Boeing 72721C · Wing Miscellaneous Structure
  > NR 0706 036 STA-PAE - CORROSION (C53-224-05) CRACK IN RT 70.85 PLUS CHORD IS CRACKED ON UPPER VERTICAL FLANGE IN RADIUS FROM BS 760 TO 770, WL 201, RBL 70.5 LONG CRACK REPAIR REQUIRED PER S/B 727-57-0112 REV 5. REPAIRED CRACK IN RT 70.8 PLUS CHORD PER EA 7-5
- [SDR 97FDEA00684](https://openairdocs.org/sdr/97FDEA00684.md): Floorbeam · cracked · Sep 25, 1997 · N144FE · Boeing 72721C · Fuselage Main, Floor Beam
  > NR 0857 035 WHILE WORKING NR 0822 DISCOVERED BS 328 FLOORBEAM WEB TO BE CRACKED T LBL 30, WL 206. REPAIRED BS 328 FLOORBEAM WEB AT LBL 30, WL 206 AS PER FED-EX SRM 51-40-2.
- [SDR 97FDEA00683](https://openairdocs.org/sdr/97FDEA00683.md): Floorbeam · corroded · Sep 25, 1997 · N144FE · Boeing 72721C · Fuselage Main, Floor Beam
  > NR 0534 034 CORROSION (C53-224-06) AROUND FASTENERS IN THE CARGO TIE DOWN PUCK ON THE BOTTOM OF UPPER FLOORBEAM CHORD AT BS 620, RBL 62.5. REPAIRED UPPER FLOORBEAM CHORD AT BS 620, RBL 15 TO RBL 70 AS PER FED SRM 53-10-8.
- [SDR 97FDEA00666](https://openairdocs.org/sdr/97FDEA00666.md): Casting · corroded · Sep 18, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous Structure
  > CORROSION (C53-224-06) IN FORWARD POCKET OF THE BARRIER NET CASTING AT RBL 1 TO RBL 8 BS 360 TO BS 380, WL 208. *S/D* REMOVED AND REPLACED BARRIER NET CASTING AT RBL 1 TO RBL 8 BS 360 TO BS 380, WL 208 PER FED-EX SRM 51-30-2. ALODINED AND PRIMED PER FED-EX S
- [SDR 97FDEA00653](https://openairdocs.org/sdr/97FDEA00653.md): Skin · corroded · Sep 12, 1997 · N144FE · Boeing 72721C · Wing, Plate/Skin
  > NR 0832 032 CORROSION (C53-224-05) ON WING CENTER TANK UPPER SKIN LBL 46, WL 192, BS 861.5 AND RBL 46, WL 192, BS 861.5. REMOVED CORROSION ON WING CENTER TANK UPPER SKIN, TOP SURFACE AT LBL 46, WL 192, BS 861.5 AND RBL 46, WL 192, BS 861.5 AND REPAIRED PER FE
- [SDR 97FDEA00650](https://openairdocs.org/sdr/97FDEA00650.md): Fitting · corroded · Sep 11, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous Structure
  > NR 0839 031 CORROSION ON HORIZONTAL SPLICE PLATE AT BS 227, WL 235, LBL 45. REMOVED AND REPLACED HORIZONTAL SPLICE PLATE AT BS 227, WL 235, LBL 45 AS PER FED-EX SRM 51-10-2, 51-10-1, 51-30-2 AND M/M 51-20-151.
- [SDR 97FDEA00629](https://openairdocs.org/sdr/97FDEA00629.md): Fitting · cracked · Sep 4, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous Structure
  > NR 0764 030 FOUND CRACK ON OUTBOARD HOLE OF STRINGER 29R, BS 1103. REMOVED CRACKED STRINGER FITTING. REPLACED WITH A NEW STRINGER FITTING AT BS 1183, STR 29R, IAW FED-EX SRM 51-30-02.
- [SDR 97FDEA00618](https://openairdocs.org/sdr/97FDEA00618.md): Floorbeam · corroded · Sep 2, 1997 · N144FE · Boeing 72721C · Fuselage Main, Floor Beam
  > NR 0822 028 CORROSION (C53-224-06) ON UPPER SURFACE OF TOP CHORD OF FLOORBEAM BS 328, LBL 29-32, WL 208. REPAIRED TOP CHORD OF FLOORBEAM BS 328 FROM LBL 9 TO LBL 63, WL 208 IAW FED-EX SRM 53-10-8.
- [SDR 97FDEA00617](https://openairdocs.org/sdr/97FDEA00617.md): Stringer · corroded · Sep 2, 1997 · N144FE · Boeing 72721C · Fuselage Main, Longeron/Stringer
  > NR 0551 029 CORROSION (C53-224-06) ON STRINGER 9 LEFT IN SEVERAL AREAS BETWEEN BS 620 AND 740. REPAIRED 59L BETWEEN BS 620-740 IAW FED 53-10-1 AND FED SRM 53-10-3.
- [SDR 97FDEA00612](https://openairdocs.org/sdr/97FDEA00612.md): Strap · corroded · Sep 2, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous Structure
  > CORROSION (C53-111-01,3) ON CENTER STABILIZER STRAP FROM BS 988 TO BS 1090, BL 0 WL 200. *S/D* REMOVED AND REPLACED BL 0 BS 950 TO 1158, WL 200 STABILIZER STRAP PER FED-EX SRM 51-10-1 AD 51-30-2.
- [SDR 97FDEA00601](https://openairdocs.org/sdr/97FDEA00601.md): Floorbeam · corroded · Sep 2, 1997 · N144FE · Boeing 72721C · Fuselage Main, Floor Beam
  > NR 0840 020 STA-PAE - WHILE WORKING NR0374 FOUND DOUBLE HOLES IN UPPER SIDE OF BS 1130 CHORD, BS 1130, RBL 32 AND 37, LBL 33 AND 38, WL 208 ALSO CORROSION AND CRACK INDICATION AT LBL 33. REPAIRED UPPER CHORD OF 1130 BEAM IAW FED-EX EA 7-5310-36165 AND EA 7-5
- [SDR 97FDEA00619](https://openairdocs.org/sdr/97FDEA00619.md): Spar Chord · corroded · Sep 1, 1997 · N144FE · Boeing 72721C · Wing Spar
  > NR 0748 027 STA-PAE - CORROSION (C57-174-01) ON BS 870 REAR SPAR UPPER CHORD RBL 20-60, LBL 10-40, WL 178. BLENDED, REMOVED CORROSION ON UPPER REAR SPAR CHORD, BS 870, RBL 20-60, LBL 10-40, WL 178. CHORD FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. RE
- [SDR 97FDEA00616](https://openairdocs.org/sdr/97FDEA00616.md): Strap · corroded · Sep 1, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous Structure
  > NR 0848 023 WHILE WORKING NR 0748 DISCOVERED CORROSION ON FWD SIDE OF WHEEL WELL BULKHEAD, TENSION LOAD STRAP AT BS 873, WL 177, RBL 65 - LBL 65. REMOVED, FABRICATED AND REPLACED TENSION STRAP AT BS 870, WL 177 FROM RBL 65 TO LBL 65 ON FWD SIDE OF WHEEL WELL
- [SDR 97FDEA00615](https://openairdocs.org/sdr/97FDEA00615.md): Bulkhead Doubler · corroded · Sep 1, 1997 · N144FE · Boeing 72721C · Fuselage Main, Bulkhead
  > NR 0851 024 WHILE WORKING NR 0748, DISCOVERED CORROSION ON FWD SIDE OF WHEEL WELL BULKHEAD RT RING DOUBLER, AT BS 873, RBL 58, WL 183. REMOVED, FABRICATED AND REPLACED RT RING DOUBLER AT BS 870, RBL 58, WL 183 IAW FED-EX DRAWING 69-14467.
- [SDR 97FDEA00614](https://openairdocs.org/sdr/97FDEA00614.md): Bulkhead Web · corroded · Sep 1, 1997 · N144FE · Boeing 72721C · Fuselage Main, Bulkhead
  > CORROSION (C57-174-01) ON BS 870 BULKHEAD WEB, RBL 70 - LBL 70, WL 178 TO 138. *S/D* BLENDED, REMOVED CORROSION ON BS 870 BULKHEAD WEB, FOUND TO BE OUT OF LIMITS PER FED SRM 53-10-1. REMOVED AND REPLACED BS 870 BULKHEAD WEB PER FED SRM 51-10-1.
- [SDR 97FDEA00613](https://openairdocs.org/sdr/97FDEA00613.md): Bulkhead Doubler · corroded · Sep 1, 1997 · N144FE · Boeing 72721C · Fuselage Main, Bulkhead
  > NR 0847 026 WHILE WORKING NR 0748, DISCOVERED CORROSION ON FWD SIDE OF WHEEL WELL BULKHEAD, LEFT RING DOUBLER AT 873, LBL 58, WL 183. REMOVED, FABRICATED AND REPLACED LEFT RING DOUBLER AT BS 870, LBL 58, WL 183 IAW FED-EX DRAWING 69-14467.
- [SDR 97FDEA00611](https://openairdocs.org/sdr/97FDEA00611.md): Spar · corroded · Sep 1, 1997 · N144FE · Boeing 72721C · Wing Spar
  > CORROSION (C57-174-01) ON BS 870 REAR SPAR LOWER CHORD, LBL 40 TO 45, WL 138. *S/D* REMOVED CORROSION, BLENDED ON BS 870 REAR SPAR LOWER CHORD. FOUND CHORD TO BE OUT OF LIMITS PER FED SRM 53-10-1. REMOVED AND REPLACED SPAR CHORD PER EA NR 7-5710-36144.
- [SDR 97FDEA00590](https://openairdocs.org/sdr/97FDEA00590.md): Stringer · corroded · Aug 27, 1997 · N144FE · Boeing 72721C · Fuselage Main, Longeron/Stringer
  > NR 0508 018 CORROSION (C53-224-02) ON STRINGER 9 LT, BS 380-460.
- [SDR 97FDEA00589](https://openairdocs.org/sdr/97FDEA00589.md): Floorbeam · corroded · Aug 27, 1997 · N144FE · Boeing 72721C · Fuselage Main, Floor Beam
  > CORROSION (C53-111-01(3)) ON LOWER CHORD OF FLOORBEAM AT BS 1130, RBL 26 TO 39, WL 200. *S/D* REPAIRED FLOORBEAM LOWER CHORD IAW FEDEX EA NR 7-5310-36166A.
- [SDR 97FDEA00582](https://openairdocs.org/sdr/97FDEA00582.md): Stringer · corroded · Aug 26, 1997 · N144FE · Boeing 72721C · Fuselage Main, Longeron/Stringer
  > CORROSION (C53-224-02) ON STRINGER 2 RT, BS 480 TO 540, BS 560 TO 580.
- [SDR 97FDEA00581](https://openairdocs.org/sdr/97FDEA00581.md): Floorbeam · corroded · Aug 26, 1997 · N144FE · Boeing 72721C · Fuselage Main, Floor Beam
  > NR 0229 017 CORROSION (C53-111-01-02) ON FLOORBEAM BS 600, WL 200, LBL 20 TO RBL 25. REPAIRED FLOORBEAM AT BS 600, WL 200, LBL 20 TO RBL 25 IAW FED-EX EA NR 7-5310-35035 REV A.
- [SDR 97FDEA00579](https://openairdocs.org/sdr/97FDEA00579.md): Floorbeam · corroded · Aug 25, 1997 · N144FE · Boeing 72721C · Fuselage Main, Floor Beam
  > CORROSION (C53-224-06) ON NOT CLIP AND DOUBLER UNDER AFT SIDE OF UPPER FLOORBEAM CHORD AT BS 740, RBL 49 AND ON PREVIOUS BLEND OUT UNDER FWD SIDE OF UPPER CHORD AT RBL 47. *S/D* REMOVED OUT OF LIMITS AREAS ON NUTCLIPS AND DOUBLER UNDER AFT SIDE OF UPPER FLOO
- [SDR 97FDEA00578](https://openairdocs.org/sdr/97FDEA00578.md): Clip · cracked · Aug 25, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous Structure
  > CRACKED STRINGER CLIP BS 970, STR 7 RT. *S/D* DRILLED OUT FASTENERS AND REMOVED CRACKED STRINGER CLIP. POSITIONED NEW STRINGER CLIP INTO PLACE AND BACKDRILL. INSTALLED FAYING SURFACES WET WITH SEALANT AND INSTALLED NEW STRINGER CLIP. ALL WORK DONE PER FED
- [SDR 97FDEA00577](https://openairdocs.org/sdr/97FDEA00577.md): Clip · cracked · Aug 25, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous Structure
  > FOUR EACH CRACKED STRINGER CLIPS AT BS 1010 AT STR 6L, 2R, 7R, 8R. *S/D* REPLACED FOUR EACH STRINGER CLIPS AT BS 1010, STR 6L, 2R, 7R AND 8R PER FED SRM 51-30-2.
- [SDR 97FDEA00576](https://openairdocs.org/sdr/97FDEA00576.md): Clip · cracked · Aug 25, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous Structure
  > TWELVE EACH CRACKED STRINGER CLIPS AT BS 990 AT STR 8L, 6L, 5L, 4L, 3L, 9R, 8R, 7R, 5R, 4R, 3R AND 2R. * S/D* REMOVED STRINGER CLIPS AND INSTALLED NEW CLIPS AT BS 990, STR 8L, 6L, 5L, 4L, 3L, 9R, 8R, 7R, 5R, 3R, AND 2R PER FED SRM 53-10-1.
- [SDR 97FDEA00575](https://openairdocs.org/sdr/97FDEA00575.md): Clip · cracked · Aug 25, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous Structure
  > CRACKED STRINGER CLIP AT BS 970 STR 5 RT. *S/D* REMOVED AND REPLACED STR CLIP AT BS 970, S5R IAW FED SRM 51-10-1 AND SRM 51-30-2.

Next page: https://openairdocs.org/deregistered/N144FE-2004-08-26/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 = 'N144FE' AND deregistration_id = 'N144FE-2004-08-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N144FE-2004-08-26/reports

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