N275FE, cancelled Aug 10, 2015

Service difficulty reports · 174

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA201003160838Transmitter · failedHYD 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 SERVIMar 16, 2010 · N275FE · Boeing 727233 · Hydraulic Quantity IndicatorSDR 08FDEA03352Skin · dentedFUSELAGE 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 FIGAug 9, 2008 · N275FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 08FDEA03351Skin · dentedFUSELAGE 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 WIAug 9, 2008 · N275FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 08FDEA03350Skin · dentedFUSELAGE 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 Aug 9, 2008 · N275FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 08FDEA03315Skin · damagedNR 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 FRAug 8, 2008 · N275FE · Boeing 727233 · Engine Air Intake SystemSDR 08FDEA03314Support Beam · crackedLT 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" BEAAug 8, 2008 · N275FE · Boeing 727233 · Wing Main, Frame StructureSDR 08FDEA03313Support Beam · crackedRT 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 ANAug 8, 2008 · N275FE · Boeing 727233 · Wing Main, Frame StructureSDR 08FDEA03192Skin · damagedEXISTING 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 98-11-03-65-18420Jul 31, 2008 · N275FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 08FDEA03164Frame · dentedFRAME 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 2-3715Jul 30, 2008 · N275FE · Boeing 727233 · Fuselage Main, FrameSDR 08FDEA03161Skin · gougedT/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-Jul 30, 2008 · N275FE · Boeing 727233 · Trailing Edge FlapsSDR 08FDEA03038Skin · delaminatedDELAM 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 Jul 24, 2008 · N275FE · Boeing 727233 · SpoilersSDR 08FDEA02883Skin · damagedGOUGE 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 SJul 15, 2008 · N275FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 08FDEA02885Skin · damagedLT 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 EDGJul 15, 2008 · N275FE · Boeing 727233 · Trailing Edge FlapsSDR 08FDEA02884Skin · gougedFUSELAGE 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.Jul 15, 2008 · N275FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 08FDEA02827Frame · damagedINTERIOR 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 Jul 11, 2008 · N275FE · Boeing 727200 · Fuselage Main, FrameSDR 08FDEA02761Skin · dentedFUSELAGE, 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 PJul 8, 2008 · N275FE · Boeing 727233 · Cargo/Baggage DoorsSDR 08FDEA02759Skin · gougedDEEP 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' Jul 8, 2008 · N275FE · Boeing 727200 · Trailing Edge FlapsSDR 08FDEA02760Skin · damagedLWR 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 NEWJul 8, 2008 · N275FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 08FDEA02190Duct · leakingAFTER 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 CABJun 7, 2008 · N275FE · Boeing 727233 · Engine Bleed Air SystemSDR 07FDEA02603Solenoid · failedAFTER 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 QRHJul 25, 2007 · N275FE · Boeing 727233 · Landing Gear Retraction/Extension SystemSDR 07FDEA02601Accessory Unit · failedAFTER 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.Jul 24, 2007 · N275FE · Boeing 727233 · Landing Gear Position and WarningSDR 06FDEA1265Clamp · out of positionAT 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 WMar 29, 2006 · N275FE · Boeing 727200 · Pneumatic Distribution SystemSDR 06FDEA0977Repair · unknownEXISTING 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 51-10Mar 7, 2006 · N275FE · Boeing 727200 · Standard Practices/StructuresSDR 06FDEA0888Repair · noneFOUND 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.Mar 2, 2006 · N275FE · Boeing 727233 · Standard Practices/StructuresSDR 06FDEA0887Repair · noneFOUND 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 FEDMar 2, 2006 · N275FE · Boeing 727233 · Standard Practices/StructuresSDR 06FDEA0886Repair · unknownFOUND 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 FMar 2, 2006 · N275FE · Boeing 727227 · Standard Practices/StructuresSDR 06FDEA0883Repair · unknownFOUND 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 WORKMMar 1, 2006 · N275FE · Boeing 727233 · Standard Practices/StructuresSDR 06FDEA0882Repair · unknownFOUND 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 WORKMar 1, 2006 · N275FE · Boeing 727233 · Standard Practices/StructuresSDR 06FDEA0881Repair · unknownFOUND 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 WORKMar 1, 2006 · N275FE · Boeing 727233 · Standard Practices/StructuresSDR 06FDEA0880Repair · unknownFOUND 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 WORKMANSMar 1, 2006 · N275FE · Boeing 727233 · Standard Practices/StructuresSDR 06FDEA0879Repair · unknownFOUND 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 WORKMar 1, 2006 · N275FE · Boeing 727233 · Standard Practices/StructuresSDR 06FDEA0878Repair · noneFOUND 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.Feb 28, 2006 · N275FE · Boeing 727200 · Aircraft StructuresSDR 06FDEA0877Repair · noneFOUND 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.Feb 28, 2006 · N275FE · Boeing 727200 · Aircraft StructuresSDR 06FDEA0876Repair · noneFOUND 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.Feb 28, 2006 · N275FE · Boeing 727200 · Aircraft StructuresSDR 06FDEA0875Repair · noneFOUND 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 Feb 28, 2006 · N275FE · Boeing 727200 · Aircraft StructuresSDR 06FDEA0873Repair · noneFOUND 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.Feb 28, 2006 · N275FE · Boeing 727200 · Aircraft StructuresSDR 06FDEA0872Repair · noneFOUND 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.Feb 28, 2006 · N275FE · Boeing 727200 · Aircraft StructuresSDR 06FDEA0871Repair · unknownFOUND 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, REFeb 28, 2006 · N275FE · Boeing 727200 · Empennage StructureSDR 06FDEA0870Repair · unknownFOUND 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 ISFeb 28, 2006 · N275FE · Boeing 727233 · Standard Practices/StructuresSDR 05FDEA00520Adc · malfunctionedREJECTED 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.Mar 15, 2005 · N275FE · Boeing 727233 · Air Data ComputerSDR 05FDEA00519Adc · malfunctionedREJECTED 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/INSTALLMar 15, 2005 · N275FE · Boeing 727233 · Air Data ComputerSDR 03FDEA01406Keelbeam · damagedLT 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 ACCESSep 3, 2003 · N275FE · Boeing 727200 · Fuselage Main, KeelSDR 03FDEA01405Frame · corrodedCORROSION 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 = .052Sep 3, 2003 · N275FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01400Skin · damagedSIX 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.Aug 29, 2003 · N275FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01390Frame · corrodedCORROSION 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.Aug 26, 2003 · N275FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA01391Panel Support · chafedVERTICAL 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 55Aug 26, 2003 · N275FE · Boeing 727200 · Vertical StabilizerSDR 03FDEA01360Frame · corrodedCORROSION (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 53-10Aug 22, 2003 · N275FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA1361Skin · damagedSIX PREVIOUSLY PLUGGED HOLES IN SKIN AT BS 400 BETWEEN STR 14 - 15 LT ADJACENT TO EXISTING FASTENERS.Aug 22, 2003 · N275FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01359Skin · dentedDENT IN SKIN BS 380 BETWEEN STR 14L AND STR 15L. CUT OUT DAMAGE, INSTALLED REPAIR DOUBLER (EXTERNAL) PER EA 7-5330-70501.Aug 22, 2003 · N275FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA01326Keelbeam · corrodedKEEL BEAM (STR 29R OUTBD FLANGE) IS CORRODED BEYOND LIMITS. REPAIRED RT KEEL BEAM OUTBD FLANGE AT BS 950F-970 PER SR 27-53-023A.Aug 15, 2003 · N275FE · Boeing 727200 · Fuselage Main, Keel
Back to N275FE, cancelled Aug 10, 2015