# Service difficulty reports: N275FE, cancelled Aug 10, 2015

A list on [N275FE, cancelled Aug 10, 2015](https://openairdocs.org/deregistered/N275FE-2015-08-10.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 · 174 reports

- [SDR FDEA201003160838](https://openairdocs.org/sdr/FDEA201003160838.md): Transmitter · failed · Mar 16, 2010 · N275FE · Boeing 727233 · Hydraulic Quantity Indicator
  > HYD SYS A QTY WENT TO ZERO WHEN GEAR RAISED AFTER TAKEOFF. PRESSURE REMAINED STEADY AT 3000 PSI. LOWERED GEAR NORMALLY QTY INDICATION RETURNED TO NORMAL AS GEAR CAME DOWN. GEAR FLAPS & SPOILERS WORKED OK. RAN QRH CK LIST WITH NO AFFECT. RELEASED FOR SERVI
- [SDR 08FDEA03352](https://openairdocs.org/sdr/08FDEA03352.md): Skin · dented · Aug 9, 2008 · N275FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN BELOW L1 DOOR CUTOUT HAS 2 SMALL DENTS BETWEEN STA 320 - 316 AND BETWEEN STR 19-20L. EVALUATED 02 DENTS BELOW L1 DOOR USING MECHANICAL MEANS AND FOUND DENTS WITHIN LIMITS, BUT DENTS ARE LESS THAN 10 INCHES FROM THE LAP SEAM IAW SRM 53-30-1 FIG
- [SDR 08FDEA03351](https://openairdocs.org/sdr/08FDEA03351.md): Skin · dented · Aug 9, 2008 · N275FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN BELOW L1 DOOR CUTOUT HAS 2 SMALL DENTS BETWEEN STA 320 - 316 AND BETWEEN STR 19 - 20L. EVALUATED 2 DENTS BELOW L1 DOOR USING MECHANICAL MEANS DENT NR 1 A: 1.9 Y:.031 A/Y: 61.2 AND DENT NR 2 A: 1.2 Y:.007 A/Y: 171.4. A/Y MEASUREMENTS ARE WI
- [SDR 08FDEA03350](https://openairdocs.org/sdr/08FDEA03350.md): Skin · dented · Aug 9, 2008 · N275FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN BELOW L1 DOOR CUTOUT HAS 2 VERTICAL DENTS AT STA 320 BETWEEN STR 17L - 19L. EVALUATED 2 DENTS AND MEASURED DENTS A: 1.0 Y:.019 A/Y 45.2 AND DENT 4 A: 2.4 Y:.053 A/Y 45.2, A/Y RATIO WITHIN LIMITS BUT DENTS ARE COMMON TO TEAR STRAP AND LESS
- [SDR 08FDEA03315](https://openairdocs.org/sdr/08FDEA03315.md): Skin · damaged · Aug 8, 2008 · N275FE · Boeing 727233 · Engine Air Intake System
  > NR 1 ENGINE NOSE COWL SKIN DAMAGED AT 9 O'CLOCK POSITION CUT OUT DAMAGE AREA DIM 4 3/4 BY 3 1/2 IAW B727 SRM 54-30-3 FIG 5. CUT OUT ACCESS HOLE DIM 5 IN ABOVE DAMAGE IAW B727 SRM 54-30-3 FIG 3. FABRICATED DOUBLER REPAIRS FROM 2024T3, 0.040 INCH AND FILLER FR
- [SDR 08FDEA03314](https://openairdocs.org/sdr/08FDEA03314.md): Support Beam · cracked · Aug 8, 2008 · N275FE · Boeing 727233 · Wing Main, Frame Structure
  > LT WING TRAILING EDGE SUPPORT BEAM CUT OUT ON SPOILER NR 7 IS CRACKED AT WBL 122 REMOVED "J" BEAM IAW B727 SRM 51-30-2. FABRICATED NEW "J" BEAM FROM BAC 1506 860 7075 T6 (DIM 81 INCHES IN LENGTH) AND TREATED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED "J" BEA
- [SDR 08FDEA03313](https://openairdocs.org/sdr/08FDEA03313.md): Support Beam · cracked · Aug 8, 2008 · N275FE · Boeing 727233 · Wing Main, Frame Structure
  > RT WING TRAILING EDGE SUPPORT BEAM CUT OUT ON SPOILER NR 8 IS CRACKED AT WBL 123 REMOVED "J" BEAM IAW B727 SRM 51-30-2 AND FABRICATED NEW "J" BEAM FROM BAC1506-860 7075-T6. APPROX DIM 81 INCHES IN LENGTH IAW B727 SRM 51-30-5 AND SRM 57-20-2 FIG 2. TREATED AN
- [SDR 08FDEA03192](https://openairdocs.org/sdr/08FDEA03192.md): Skin · damaged · Jul 31, 2008 · N275FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > EXISTING TOOL MARKS ON SKIN AT FUSELAGE STA 334 BY UNDER HAT SECTION AREA OF STR 10R. BLENDED OUT DAMAGE IAW SRM 51-10-1, AND FOUND OUT OF LIMITS IAW SRM 53-30-1 FIG 1 AND 2. REPAIRED SKIN IAW EA 7-5330-122358-FUSELAGE, AD 2002-07-09 AND AD 98-11-03-65-18420
- [SDR 08FDEA03164](https://openairdocs.org/sdr/08FDEA03164.md): Frame · dented · Jul 30, 2008 · N275FE · Boeing 727233 · Fuselage Main, Frame
  > FRAME AT STA 344 DENTED AT STR 5L AT 9G BULKHEAD. CUT OUT DAMAGE FROM FRAME IAW SRM 53-10-4 FIG 2. FABRICATED NEW FRAME REPAIR AND REPAIR FILLER IAW SRM 53-10-4 FIG 2 AND 53-10-2 FIG 3 AND 51-20-1. HEAT TREATED FRAME REPAIR IAW FAS ENGINEERING REPORT 2-3715
- [SDR 08FDEA03161](https://openairdocs.org/sdr/08FDEA03161.md): Skin · gouged · Jul 30, 2008 · N275FE · Boeing 727233 · Trailing Edge Flaps
  > T/E OF LT OB FOREFLAP HAS (2) EA DEEP GOUGES ON UPPER SURFACE. REMOVED DAMAGED AREA IAW SRM 51-40-20 PAGE 12. FABRICATED FILLER AND DOUBLER IAW SRM 51-40-20 PAGE 59. HOT BONDED FILLER AND DOUBLER ON SEALED EDGES AND PRIMED AREA IAW SRM 51-40-20 PARAGRAPH 7-
- [SDR 08FDEA03038](https://openairdocs.org/sdr/08FDEA03038.md): Skin · delaminated · Jul 24, 2008 · N275FE · Boeing 727233 · Spoilers
  > DELAM SPOTS TOP NR 2 SPOILER REMOVED DAMAGE AREAS, CLEANED AND PREP IAW B727 SRM 51-40-20 PG 12-14,42-47. FABRICATED REPAIR FILLERS (2) APPROX 7 BY 5, 22 BY 3 AND REPAIR DOUBLERS (2) APPROX 10 BY 6.5 AND 25 BY 4.5 USING.025 7075 T6 IAW B727 SRM 51-40-20 PG
- [SDR 08FDEA02883](https://openairdocs.org/sdr/08FDEA02883.md): Skin · damaged · Jul 15, 2008 · N275FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > GOUGE IN SKIN AT FUSELAGE STA 265 FWD OF ELEC POWER RECEPTACLE ACCESS DOOR TRIMMED OUT DAMAGE SKIN (DIM 4 BY 1 1/4) IAW EA 7-5330-122320. HFEC INSPECTED AREA IAW NDTM 51-00-00 FIG 16 AND 2. NO DEFECTS NOTED. FABRICATED REPAIR DOUBLER AND REPAIR FILLER IAW S
- [SDR 08FDEA02885](https://openairdocs.org/sdr/08FDEA02885.md): Skin · damaged · Jul 15, 2008 · N275FE · Boeing 727233 · Trailing Edge Flaps
  > LT WING T/E O/B FOREFLAP HAS DEEP GOUGE ON UPPER SURFACE AT WS 450. REMOVED DAMAGED AREA IAW B727 SRM 51-40-20 PARAGRAPH 12 AND FABRICATED FILLER AND DOUBLER FROM 2024T3.016 (3 BY 3) AREA IAW B727 SRM 51-40-20 GAUGE 59. BONDED FILLER AND DOUBLER, SEALED EDG
- [SDR 08FDEA02884](https://openairdocs.org/sdr/08FDEA02884.md): Skin · gouged · Jul 15, 2008 · N275FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERIOR SKIN GOUGED STA 1090 STR 22R. BLENDED OUT DAMAGE AND FOUND OUT OF LIMITS IAW SRM 51-10-1 AND 53-30-1 FIG 1 AND 2. REPAIRED SKIN FUSELAGE STA 1090 STRINGER 22R IAW EA 7-5330-122334.
- [SDR 08FDEA02827](https://openairdocs.org/sdr/08FDEA02827.md): Frame · damaged · Jul 11, 2008 · N275FE · Boeing 727200 · Fuselage Main, Frame
  > INTERIOR FUSELAGE STA 344 STRINGER TIE AT STR 7R HAS 02 FASTENERS WITH "O" ED. REMOVED STRINGER TIE IAW B727 SRM 51-30-2, CUT OUT DAMAGE FRAME DIM 1.5 X 5/8 IAW B727 SRM 53-10-4 FIG 2. FABRICATED NEW STRINGER TIE FROM 7075T6.032 DIM 3 X 3.75. FRAME REPAIR
- [SDR 08FDEA02761](https://openairdocs.org/sdr/08FDEA02761.md): Skin · dented · Jul 8, 2008 · N275FE · Boeing 727233 · Cargo/Baggage Doors
  > FUSELAGE, C-3 DOOR HAS NUMEROUS DENTS AND BULGES ON EXTERIOR SKIN OF DOOR REMOVED C-3 DOOR ASSY AND HANDLE IAW MM 52-35-051-4 AND SRM 51-30-2. REMOVED, FABRICATED AND INSTALLED NEW C-3 DOOR SKIN IAW EA 7-5230-22339. REINSTALLED C-3 DOOR HANDLE AND ATTACHED P
- [SDR 08FDEA02759](https://openairdocs.org/sdr/08FDEA02759.md): Skin · gouged · Jul 8, 2008 · N275FE · Boeing 727200 · Trailing Edge Flaps
  > DEEP GOUGE IN LT O/B FOREFLAP, L/E CAP UPPER SURFACE APPROX 10 INCHES FROM I/B END IN PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA DIM 1' X 5/8 IAW B727 SRM 57-50-4 FIG 1. FABRICATED REPAIR PLATE MAT USED 2024T3.063'
- [SDR 08FDEA02760](https://openairdocs.org/sdr/08FDEA02760.md): Skin · damaged · Jul 8, 2008 · N275FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > LWR FUSELAGE, DRAIN HOLE DAMAGED AT STA. 355 STR 30. REMOVED SKIN PANEL IAW B727 SRM 51-30-2. FABRICATED NEW SKIN MAT USED 2024T3.050 (27 BY 8.75) IAW B727 SRM 53-30-2 FIG 2 AND 51-30-5. TREATED AND PRIMED NEW SKIN AREA IAW B727 SRM 51-10-2. INSTALLED NEW
- [SDR 08FDEA02190](https://openairdocs.org/sdr/08FDEA02190.md): Duct · leaking · Jun 7, 2008 · N275FE · Boeing 727233 · Engine Bleed Air System
  > AFTER TAKEOFF IN CLIMB-OUT NR 3 ENG STRUT OVERHEAT ILLUM. RAN QRH WHICH DETERMINED POSSIBLE LEAK ON FUSELAGE SIDE. WITH LIGHT EXTINGUSHED CONT CLIMB AND CABIN PRESSURE WOULD NOT HOLD AT FL 320 WITH ONE PACK OPERATION. REQ DESCENT TO 10,000 FT TO CONTROL CAB
- [SDR 07FDEA02603](https://openairdocs.org/sdr/07FDEA02603.md): Solenoid · failed · Jul 25, 2007 · N275FE · Boeing 727233 · Landing Gear Retraction/Extension System
  > AFTER LIFTOFF AND GEAR RETRACTION LANDING GEAR LEVER WOULD NOT RAISE PAST THE OFF POSITION. THE LEVER LATCH LIGHT CIRCUIT BREAKER IMMEDIATELY OPENED AND THE FORWARD LANDING GEAR ANNUNCIATOR PANEL LIGHTS INDICATED ONLY THE GREEN NOSE GEAR LIGHT. CONSULT QRH
- [SDR 07FDEA02601](https://openairdocs.org/sdr/07FDEA02601.md): Accessory Unit · failed · Jul 24, 2007 · N275FE · Boeing 727233 · Landing Gear Position and Warning
  > AFTER LOWERING LANDING GEAR, DID NOT GET LEFT OR RIGHT GEAR DOWN LIGHTS. COMPLIED WITH QRH PROCEDURES TO VERIFY GEAR DOWN AND LOCKED. NORMAL LANDING ACCOMPLISHED. REMOVED AND REPLACED LANDING GEAR POSITION/WARNING ACCESSORY UNIT IAW 727-200 AMM 32-09-122-5.
- [SDR 06FDEA1265](https://openairdocs.org/sdr/06FDEA1265.md): Clamp · out of position · Mar 29, 2006 · N275FE · Boeing 727200 · Pneumatic Distribution System
  > AT FLT LEVEL 320 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED, WENT TO QRH TURNED RIGHT PACK SWITCH OFF, LIGHT STILL ON. CLOSED NR 3 BLEED LIGHT STILL ON. CLOSED CARGO HEAT SWITCH LIGHT STILL ON. WHEN NR 3 THRUST LEVER RETARDED LIGHT WENT OUT. WING ANTI-ICE W
- [SDR 06FDEA0977](https://openairdocs.org/sdr/06FDEA0977.md): Repair · unknown · Mar 7, 2006 · N275FE · Boeing 727200 · Standard Practices/Structures
  > EXISTING REPAIR STA 720-745 STR 21L-22L IS IAW EXISTING FAA DATA. REPLACE EXISTING REPAIR PER SRM. FABRICATED AND INSTALLED NEW DOUBLER AND FILLER FROM 2024- T3.063 BATCH 1022264 IAW SRM 53-30-3 FIG 2, 4 & 51-30-2, TREATED, PRIMED AND PAINTED IAW SRM 51-10
- [SDR 06FDEA0888](https://openairdocs.org/sdr/06FDEA0888.md): Repair · none · Mar 2, 2006 · N275FE · Boeing 727233 · Standard Practices/Structures
  > FOUND 3 REPAIRS LOCATED ON NR 3 CARGO DOOR OUTER SKIN, REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIRS WERE ACCOMPLISHED USING FAA APPROVED DATA. REPAIRS FOUND TO BE IAW SRM 52-00-3 FIG 3. REPAIRS CLASSIFIED AS MAJOR.
- [SDR 06FDEA0887](https://openairdocs.org/sdr/06FDEA0887.md): Repair · none · Mar 2, 2006 · N275FE · Boeing 727233 · Standard Practices/Structures
  > FOUND REPAIR LOCATED ON RIGHT WING L/E ABOVE THE NR 4 KRUGER FLAP REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR FOUND TO IAW SRM 57-30-4 FIG 2. REPAIR CLASSIFIED AS MAJOR IAW FED
- [SDR 06FDEA0886](https://openairdocs.org/sdr/06FDEA0886.md): Repair · unknown · Mar 2, 2006 · N275FE · Boeing 727227 · Standard Practices/Structures
  > FOUND 2 REPAIRS LOCATED ON THE RIGHT L/E WING UPPER SURFACE STA 450 AND 460. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIRS WERE DETERMINED TO BE IAW SRM 57-30-4 F
- [SDR 06FDEA0883](https://openairdocs.org/sdr/06FDEA0883.md): Repair · unknown · Mar 1, 2006 · N275FE · Boeing 727233 · Standard Practices/Structures
  > FOUND PREVIOUSLY REPAIR INSTALLED AT STA 400 STR 17L-18L WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 53-30-3 FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL THICKNESS AND TYPE, FASTENER SPACING AND NUMBER, GENERAL WORKM
- [SDR 06FDEA0882](https://openairdocs.org/sdr/06FDEA0882.md): Repair · unknown · Mar 1, 2006 · N275FE · Boeing 727233 · Standard Practices/Structures
  > FOUND PREVIOUSLY REPAIR INSTALLED AT STA 188 STR 21R WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 53-30-3 FIG 5, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORK
- [SDR 06FDEA0881](https://openairdocs.org/sdr/06FDEA0881.md): Repair · unknown · Mar 1, 2006 · N275FE · Boeing 727233 · Standard Practices/Structures
  > FOUND PREVIOUSLY REPAIR INSTALLED AT STA 1030 STR 18L-19L WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 53-30-3 FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL THICKNESS AND TYPE, FASTENER SPACING AND NUMBER, GENERAL WORK
- [SDR 06FDEA0880](https://openairdocs.org/sdr/06FDEA0880.md): Repair · unknown · Mar 1, 2006 · N275FE · Boeing 727233 · Standard Practices/Structures
  > FOUND PREVIOUSLY REPAIR INSTALLED AT STA 720E STR 19L WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 53-30-3, FIG 4 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL THICKNESS AND TYPE, FASTENER SPACING AND NUMBERS, GENERAL WORKMANS
- [SDR 06FDEA0879](https://openairdocs.org/sdr/06FDEA0879.md): Repair · unknown · Mar 1, 2006 · N275FE · Boeing 727233 · Standard Practices/Structures
  > FOUND PREVIOUSLY REPAIR INSTALLED AT STA 1050 STR 27R-28R WAS DETERMINED TO BE ACCOMPLISHED PER SRM 53-30-3 FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL THICKNESS AND TYPE, FASTENER SPACING AND NUMBERS, GENERAL WORK
- [SDR 06FDEA0878](https://openairdocs.org/sdr/06FDEA0878.md): Repair · none · Feb 28, 2006 · N275FE · Boeing 727200 · Aircraft Structures
  > FOUND REPAIR AT STA 990 STR 27R, REPAIR REQUIRES EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA PER FEDEX EA 7-5310-27778. REPAIR CLASSIFIED AS MAJOR.
- [SDR 06FDEA0877](https://openairdocs.org/sdr/06FDEA0877.md): Repair · none · Feb 28, 2006 · N275FE · Boeing 727200 · Aircraft Structures
  > FOUND REPAIR LOCATED AT STA 700 STR 28L REPAIR REQUIRES EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA PER FEDEX EA 7-5310-02879.
- [SDR 06FDEA0876](https://openairdocs.org/sdr/06FDEA0876.md): Repair · none · Feb 28, 2006 · N275FE · Boeing 727200 · Aircraft Structures
  > FOUND REPAIR LOCATED AT STA 1130 STR 5L, REPAIR REQUIRES EVALUATION FOR MAJOR / MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA PER FEDEX EA 7-5330-56270.
- [SDR 06FDEA0875](https://openairdocs.org/sdr/06FDEA0875.md): Repair · none · Feb 28, 2006 · N275FE · Boeing 727200 · Aircraft Structures
  > FOUND REPAIR LOCATED AT STA 630 STR 27L REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION, AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA PER FEDEX EA 5330-B27- 20619. REPAIR CLASSIFIED AS
- [SDR 06FDEA0873](https://openairdocs.org/sdr/06FDEA0873.md): Repair · none · Feb 28, 2006 · N275FE · Boeing 727200 · Aircraft Structures
  > FOUND REPAIR LOCATED AT STA 400 STR 15L REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR ACCOMPLISHED USING FAA APPROVED DATA PER FEDEX EA 7-5330-70501. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR 06FDEA0872](https://openairdocs.org/sdr/06FDEA0872.md): Repair · none · Feb 28, 2006 · N275FE · Boeing 727200 · Aircraft Structures
  > FOUND REPAIR LOCATED AT STA 380 STR 15L REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR ACCOMPLISHED USING FAA APPROVED DATA ON FEDEX EA 7-5330-70501. REPAIR IS CLASSIFIED AS MAJOR.
- [SDR 06FDEA0871](https://openairdocs.org/sdr/06FDEA0871.md): Repair · unknown · Feb 28, 2006 · N275FE · Boeing 727200 · Empennage Structure
  > FOUND PREVIOUSLY REPAIR INSTALLED ON UPPER RUDDER TRAILING EDGE WAS ACCOMPLISHED IAW SRM 51-40-9, FIG 1 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP, RE
- [SDR 06FDEA0870](https://openairdocs.org/sdr/06FDEA0870.md): Repair · unknown · Feb 28, 2006 · N275FE · Boeing 727233 · Standard Practices/Structures
  > FOUND PREVIOUSLY REPAIR INSTALLED AT STA 540 STR 27R WAS ACCOMPLISHED PER FEDEX EA 7-5330-85285, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP, REPAIR IS
- [SDR 05FDEA00520](https://openairdocs.org/sdr/05FDEA00520.md): Adc · malfunctioned · Mar 15, 2005 · N275FE · Boeing 727233 · Air Data Computer
  > REJECTED TAKEOFF. REMOVED AND REPLACED AIR DATA COMPUTER IAW MM 34-12-011-4. GRD CK OK. A/C DOWN GRADED TO NOT CAT II. A/P NR 1 CK CAT II A/P NR 2 CK CAT II PREMATURE REMOVAL/INSTALLATION OFF MFG HG480B13.
- [SDR 05FDEA00519](https://openairdocs.org/sdr/05FDEA00519.md): Adc · malfunctioned · Mar 15, 2005 · N275FE · Boeing 727233 · Air Data Computer
  > REJECTED TO AT 80 KTS. RAN RTO CHECKLIST. NO AIRSPEED ON CAPT'S AIRSPEED INDICATOR. REMOVED AND REPLACED AIR DATA COMPUTER IAW MM 34-12-011-4. A/C DOWN GRADED TO NOT CAT II. A/P NR 1 CK CAT II A/P NR 2 CK CAT II. R/I FROM FACT PREMATURE REMOVAL/INSTALL
- [SDR 03FDEA01406](https://openairdocs.org/sdr/03FDEA01406.md): Keelbeam · damaged · Sep 3, 2003 · N275FE · Boeing 727200 · Fuselage Main, Keel
  > LT KEEL BEAM AT STA 740 HAS DAMAGED HOLE DUE TO A SEIZED FASTENER IN KEELBEAM. REMOVED AND REPLACED DAMAGED LT KEELBEAM STA 740 IAW FED EX EA 7-5330-54955, DWG 65-54577-21, AND SRM 53-30-3 FIG. 3. LEAK CHECK GOOD ON DISTRIBUTION DUCTS. REMOVED FOR ACCES
- [SDR 03FDEA01405](https://openairdocs.org/sdr/03FDEA01405.md): Frame · corroded · Sep 3, 2003 · N275FE · Boeing 727200 · Fuselage Main, Frame
  > CORROSION ON 740 FRAME COMMON TO DELTA BOX RBL 7 THRU LBL 7 WL 156 REMOVED CORROSION ON 740 FRAME COMMON TO DELTA BOX RBL 7 TO LBL 7, WL 156. CORROSION BLEND-OUT OUT OF LIMITS IAW SRM 53-10-1 FIG 1. ORIGINAL THICKNESS.112 MATERIAL REMAINING =.052
- [SDR 03FDEA01400](https://openairdocs.org/sdr/03FDEA01400.md): Skin · damaged · Aug 29, 2003 · N275FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > SIX PREVIOUSLY PLUGGED HOLES IN SKIN AT BS 400 BETWEEN STR 14 - 15 LT ADJACENT TO EXISTING FASTENERS. BS 400 SKIN AREA BETWEEN STR 14-15 LT WITH PLUGGED HOLES WAS REPAIRED PER FED EX EA 7-5330-70501.
- [SDR 03FDEA01390](https://openairdocs.org/sdr/03FDEA01390.md): Frame · corroded · Aug 26, 2003 · N275FE · Boeing 727200 · Fuselage Main, Frame
  > CORROSION ON FRAME STA 950E BETWEEN STR 28L & 29L. REPAIRED FRAME BS 950E, STR 28L-29L IAW SRM 53-10-4 FIG 13 AND EA 7-5310-54947.
- [SDR 03FDEA01391](https://openairdocs.org/sdr/03FDEA01391.md): Panel Support · chafed · Aug 26, 2003 · N275FE · Boeing 727200 · Vertical Stabilizer
  > VERTICAL STAB LT TEE SUPPORT IS CHAFED WHERE PANEL 8603 LWR ATTACHMENT ANGLE, ATTACHES TO THE PANEL SUPPORT. CUT OUT DAMAGED AREA 3 X 1 INCH ON LT VERTICAL STAB SUPPORT AT PANEL 9603'S AFT ATTACH ANGLE MOUNT HOLE. FABRICATED AND INSTALLED REPAIR IAW SRM 55
- [SDR 03FDEA01360](https://openairdocs.org/sdr/03FDEA01360.md): Frame · corroded · Aug 22, 2003 · N275FE · Boeing 727200 · Fuselage Main, Frame
  > CORROSION (C53-113-01, 2) ON FRAME STA 970 BETWEEN STR 28L & 29L. CORROSION ON FRAME BS 970, STR 28L-29L WAS FOUND OUT OF LIMITS PER SRM 53-10-1. REMOVED DAMAGED FRAME SECTION AT SHEAR TIE SKIN ATTACHMENT, FABRICATED REPAIR PARTS, AND INSTALLED PER SRM 53-10
- [SDR 03FDEA1361](https://openairdocs.org/sdr/03FDEA1361.md): Skin · damaged · Aug 22, 2003 · N275FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > SIX PREVIOUSLY PLUGGED HOLES IN SKIN AT BS 400 BETWEEN STR 14 - 15 LT ADJACENT TO EXISTING FASTENERS.
- [SDR 03FDEA01359](https://openairdocs.org/sdr/03FDEA01359.md): Skin · dented · Aug 22, 2003 · N275FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > DENT IN SKIN BS 380 BETWEEN STR 14L AND STR 15L. CUT OUT DAMAGE, INSTALLED REPAIR DOUBLER (EXTERNAL) PER EA 7-5330-70501.
- [SDR 03FDEA01326](https://openairdocs.org/sdr/03FDEA01326.md): Keelbeam · corroded · Aug 15, 2003 · N275FE · Boeing 727200 · Fuselage Main, Keel
  > KEEL BEAM (STR 29R OUTBD FLANGE) IS CORRODED BEYOND LIMITS. REPAIRED RT KEEL BEAM OUTBD FLANGE AT BS 950F-970 PER SR 27-53-023A.

Next page: https://openairdocs.org/deregistered/N275FE-2015-08-10/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 = 'N275FE' AND deregistration_id = 'N275FE-2015-08-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N275FE-2015-08-10/reports

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