# Service difficulty reports: N498FE, cancelled Mar 19, 2013

A list on [N498FE, cancelled Mar 19, 2013](https://openairdocs.org/deregistered/N498FE-2013-03-19.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 FDEA201010013850](https://openairdocs.org/sdr/FDEA201010013850.md): Connector · failed · Oct 1, 2010 · N498FE · Boeing 727232 · Fire Protection System Wiring
  > 30 SECONDS AFTER TAKE OFF CARGO SMOKE WARNING OCCURED. BELLS AND LIGHTS FOR ABOUT 3 SECONDS THEN WENT OUT. 10 SECONDS LATER WARNING OCCURED AGAIN AND LASTED FOR ABOUT 10 SECONDS AND THEN STOPPED AGAIN. REINSTALLED CONNECTOR PLUGS ON NR 1 AND NR 2 LWR CARG
- [SDR FDEA201009243702](https://openairdocs.org/sdr/FDEA201009243702.md): Fire Detector · false activation · Sep 24, 2010 · N498FE · Boeing 727232 · Fire Detection
  > ON TAKEOFF APPROX 1000' AGL GOT AN INTERMITTENT FIREBELL AND S/O SAW CARGO SMOKE WARNING LOWER FWD CARGO ON, THEN THE LIGHT WENT OUT. AML REFLECTED A PREVIOUS WRITEUP ON THE SAME SYS. DEEMED TO RETURN AND LAND IMMEDIATELY. REMOVED SMOKE DETECTORS 1,2,3, &
- [SDR FDEA200907252750](https://openairdocs.org/sdr/FDEA200907252750.md): Connector · shorted · Jul 25, 2009 · N498FE · Boeing 727232 · Air Conditioning System Wiring
  > DURING CLIMB, ACFT CABIN ACT WAS TOO HIGH. FOUND PACK VALVE C/B POPPED. CABIN ALT STABILIZED AT 8500' AT 20,000 WITH L AFT PACK OPERATING ONLY. TROUBLESHOT SYS, FOUND PACK VALVE BREAKER WOULD RESET MOMENTARILY. CHECKED BOTH FWD PACK SHUTOFF VALVES NO DEFE
- [SDR 08FDEA01789](https://openairdocs.org/sdr/08FDEA01789.md): Stringer Clip · cracked · May 7, 2008 · N498FE · Boeing 727232 · Fuselage Main, Attach Fittings
  > ORIGINAL LOST, A86-143 REF AD 92-12-03, AFT PIT BILGE BODY FRAME STR CLIP IS BUCKLED, CRACKED, CORRODED BS 950F, STR 27L (EO 7-5310-7-2354) N00252. REMOVED AND REPLACED STR CLIP AT AFT PIT BILGE BODY FRAME STR 27L, STA 950F, REF SRM 51-30-2 PG 2-4. THIS IS
- [SDR 08FDEA01746](https://openairdocs.org/sdr/08FDEA01746.md): Fairing · cracked · May 3, 2008 · N498FE · Boeing 727232 · Trailing Edge Flaps
  > LEFT WING INBOARD MID FLAP OUTBOARD JACK SCREW FAIRING INTERIOR SKIN CRACKED AT ATTACH HOLE REPAIRED LEFT WING INBD MID FLAP O/B JACK SCREW FAIRING REF SRM 57-20-4 PG 5 AND SRM 51-30-2 PG 2. THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 08FDEA01713](https://openairdocs.org/sdr/08FDEA01713.md): Stringer Splice · corroded · May 1, 2008 · N498FE · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > FWD PIT STRINGER SPLICE AT 27L GOING THROUGH STA 680 CORRODED ON OUTBD SIDE REMOVED CORROSION FROM ORIGINAL THICKNESS OF 0.064 INCH FROM BUTT SPLICE STRAP WITH 0.054" REMAINING. OUT-OF-LIMITS DUE TO "NO REWORK PERMITTED IN BUTT SPLICE STRAP". FABRICATED REPA
- [SDR 08FDEA01705](https://openairdocs.org/sdr/08FDEA01705.md): Stop Fitting · gouged · Apr 30, 2008 · N498FE · Boeing 727232 · Cargo/Baggage Doors
  > AFT LOWER NR 3 CARGO DOOR FORWARD FRAME LOWER STOP FITTING GOUGED. DOOR REMOVED REF AMM 52-35-071-4, LWR FORWARD FITTING REMOVED AND INSTALLED REF SRM 51-30-02. DOOR INSTALLED REF AMM 52-35-071, ADJUSTED STOPS. THIS IS CLASSIFIED AS A MAJOR REPAIR.
- [SDR 08FDEA01704](https://openairdocs.org/sdr/08FDEA01704.md): Rib · cracked · Apr 30, 2008 · N498FE · Boeing 727232 · Horizontal Stabilizer, Spar/Rib
  > RT HORIZONTAL STAB, AFT SUPPORT RIB IS CRACKED NEAR ELEVATOR ATTACH POINT, ELEVATOR STA 99.79 REMOVED WIPER PLATES, REF SRM 51-30-2. FAB RADIUS FILLER FOR REPAIR,.100" 2024-T3 REF DWG 69-33174. TREATED AND PRIMED REF SRM 51-10-2. INSTALLED REPAIR REF SRM 5
- [SDR 08FDEA01700](https://openairdocs.org/sdr/08FDEA01700.md): Skin · cracked · Apr 30, 2008 · N498FE · Boeing 727232 · Passenger/Crew Doors
  > MAIN DECK 1R DOOR EXT SKIN IS BUCKLED/CRACKED AT UPPER HINGE CUT OUT UPPER EDGE, 4 INCHES FROM FWD END. REMOVED DAMAGE AND CHECKED WITH HFEC, NO DEFECTS FOUND. REMOVED LINER SUPPORT, VERIFIED MATERIAL, MADE A.040 INSURANCE CUT REF SRM 52-00-3 FIG 3 STEP 2.
- [SDR 08FDEA01697](https://openairdocs.org/sdr/08FDEA01697.md): Web · corroded · Apr 30, 2008 · N498FE · Boeing 727232 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB TO BODY SKIN ON ANGLE ON WEB BETWEEN BS 950A TO 950B, LBL 18, WL 141 REPLACED WEB AT STA 950 - 950B, LBL AND CLIP AT STA 950A LBL 18 REF BOEING DWG 69-44877 AND SRM 51-30-3. THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 08FDEA01696](https://openairdocs.org/sdr/08FDEA01696.md): Panel · delaminated · Apr 30, 2008 · N498FE · Boeing 727232 · Wing, Plate/Skin
  > RIGHT WING L/E LWR PANEL 6402 HAS 2 INCH BY 6 INCH AREA OF DISBOND CORE FROM INNER AND OUTER SURFACES. REPAIRED PANEL 6402 REF SRM 51-40-9 PARAGRAPHS 3D, 4B, 4E, 4F AND AMM 51-20-051-7, 51-20-151-7 TAP TEST GOOD. THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 08FDEA01695](https://openairdocs.org/sdr/08FDEA01695.md): Structure · cracked · Apr 30, 2008 · N498FE · Boeing 727232 · Fuselage Miscellaneous Structure
  > LWR EXT FUSE WING BODY FILLET FAIRING SUPPORT FRAME LWR CHORD ANGLE IS BUCKLED/CRACKED AT I/B END 950A, LBL 14. REPAIRED SUPPORT FRAME LOWER CHORD ANGLE FOR WING TO BODY FAIRING AT 950A, LBL 14 REF SRM 51-40-3. THIS IS CLASSIFIED AS A MINOR.
- [SDR 08FDEA01496](https://openairdocs.org/sdr/08FDEA01496.md): Skin · dented · Apr 23, 2008 · N498FE · Boeing 727232 · Elevator, Plate/Skin
  > RT ELEVATOR LWR SKIN HAS A DENT 97 INCHES FROM I/B EDGE, 7 INCHES FWD OF REAR SPAR. MEASURED DENT FOUND TO BE WITHIN LIMITS, MEASURED DENT Y =.040 A = 4 INCHES FOUND TO BE 100 REF SRM 55-10-1 PG 7 FIG 2. THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 08FDEA01495](https://openairdocs.org/sdr/08FDEA01495.md): Skin · cracked · Apr 23, 2008 · N498FE · Boeing 727232 · Fuselage Main, Plate/Skin
  > MLG WW KEEL BEAM LWR EXT SKIN PANEL AT BS 940 TO 950-12, LBL 5-RBL 5 2 EA CRACKED FASTENER HOLES BS 947, RBL 5 (MKD). REMOVED DAMAGE AND FABRICATED A REPAIR FILLER AND A REPAIR DOUBLER. TREATED, PRIMED AND PAINTED ALL REPAIR PARTS AND INSTALLED. EDGE SEALED
- [SDR 08FDEA01494](https://openairdocs.org/sdr/08FDEA01494.md): Skin · corroded · Apr 23, 2008 · N498FE · Boeing 727232 · Fuselage Main, Plate/Skin
  > MLG W/W KEEL BEAM LWR EXT SKIN PANEL AT BS 940 TO 950 PLUS 12, LBL 5- RBL 5 HAS SEVERAL AREAS OF CORROSION REMOVED AREAS OF CORROSION. REMOVED 0.005 INCH FROM ORIGINAL SKIN THICKNESS OF 0.071 INCH. 0.066 INCH REMAINING AND SKIN PANEL IS WITHIN LIMITS. TRE
- [SDR 08FDEA01493](https://openairdocs.org/sdr/08FDEA01493.md): Stringer Clip · corroded · Apr 23, 2008 · N498FE · Boeing 727232 · Fuselage Main, Attach Fittings
  > STRINGER TIE ON STR 26R AT FS 941A HAS CORROSION ON OUTER SIDE OF TIE. REMOVED DAMAGED STRINGER TIE REPLACED NEW STRINGER TIE, REF SRM 51-30-2 PG1. THIS IS CLASSIFIED AS A MAJOR REPAIR.
- [SDR 08FDEA01489](https://openairdocs.org/sdr/08FDEA01489.md): Shear Tie · corroded · Apr 23, 2008 · N498FE · Boeing 727232 · Fuselage Internal Mounting Structure
  > FWD PIT SHEAR TIE STA 520 BETWEEN STR 28L-28R CORRODED. REMOVED FASTENER'S TO ACCESS CORROSION IN REF TO SRM 51-30-2 PG 2. REMOVED CORROSION ON FWD SIDE OF SHEAR TIE BS 520 STR 28L-28R IN REF TO SRM 53-10-1. CHECK SHEAR TIE FOR MAT'L LOSS ORIGINAL THICKNE
- [SDR 08FDEA01488](https://openairdocs.org/sdr/08FDEA01488.md): Structure · cracked · Apr 23, 2008 · N498FE · Boeing 727232 · Nacelle/Pylon, Plate/Skin
  > NR 2 ENGINE LEFT FWD COWLING OUTER AFT CORNER MULTIPLE LAYERS OF SHEET METAL ARE CRACKED. REMOVED DAMAGED AREA REF SRM 51-40-2. MATERIAL ID AT 2024 T3.080 REF SRM 65-10-3 A48140 FOR DOUBLER. MATERIAL ID AT 2024 T3.100 A 11734 REF SRM 54-30-2 FOR FILLER.
- [SDR 08FDEA01486](https://openairdocs.org/sdr/08FDEA01486.md): Fairing · cracked · Apr 23, 2008 · N498FE · Boeing 727200 · Wing Miscellaneous Structure
  > RT WING NR 6 FLAP TRACK FWD FAIRING HAS SEVERAL CRACKS REMOVED FASTENERS AND FABRICATED NEW REPAIR DOUBLER. INSTALLED NEW DOUBLER REF SRM 57-20-4 FIG 1. TREATED AND PRIMED AND PAINTED REF SRM 51-10-2 P2. THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 08FDEA01485](https://openairdocs.org/sdr/08FDEA01485.md): Bulkhead · corroded · Apr 23, 2008 · N498FE · Boeing 727232 · Fuselage Main, Bulkhead
  > BS 178 BULKHEAD EXT SURFACE WL 187 - 193 LBL 19" TO 24" HAS CORROSION PITS. CHEMICALLY REMOVED CORROSION FROM BS 178 BULKHEAD EXT SURFACE WL 185-193 LBL 19" TO 24". THICKNESS OF MATERIAL IS.055, MATERIAL REMAINING IS.053 A LOSS OF.022 FOUND TO BE WITH-IN L
- [SDR 08FDEA01484](https://openairdocs.org/sdr/08FDEA01484.md): Angle · corroded · Apr 23, 2008 · N498FE · Boeing 727232 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB TO BODY SKIN ANGLE ON WEB BETWEEN BS 950A TO 950B, RBL 3, WL 139. REMOVED AND REPLACED INTERCOSTAL WEB AND AFT ATTACH CLIP REF 51-30-2 PG 8. THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 08FDEA01482](https://openairdocs.org/sdr/08FDEA01482.md): Fitting · cracked · Apr 23, 2008 · N498FE · Boeing 727232 · Fuselage Main, Attach Fittings
  > MAIN DECK 1R DR BOTTOM CROSS BEAM AFT STOP FITTING IS CRACKED REMOVED AND REPLACED STOP FITTING REF SRM 51-30-2. DOOR ADJUSTEMENT ACCOMPLISED ON W/0 40304 N00067, THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 08FDEA01481](https://openairdocs.org/sdr/08FDEA01481.md): Skin · gouged · Apr 23, 2008 · N498FE · Boeing 727232 · Fuselage Main, Plate/Skin
  > EXT FUSELAGE SKIN IS GOUGED AT BS 670 O/B OF STR S-28L REMOVED DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER REPAIR REF SRM-30-3 FIG 1. THIS IS CLASSIFIED AS A MAJOR REPAIR AND A CATEGORY "B" REPAIR.
- [SDR 08FDEA01480](https://openairdocs.org/sdr/08FDEA01480.md): Intercostal · cracked · Apr 23, 2008 · N498FE · Boeing 727232 · Fuselage Miscellaneous Structure
  > MAIN DECK 1R DR CROSS BEAM, INTERCOSTAL I/B FLANGE IS CRACKED AT 4TH BEAM FROM BOTTOM, 13 INCHES FROM FWD END. REMOVED OLD INTERCOSTAL 4TH FROM BOTTOM 13 INCHES FROM FWD END. HAD SHOP FABRICATE N00557. DRILLED NEW INTERCOSTAL, INSTALLED INTERCOSTAL TREATED
- [SDR 08FDEA01458](https://openairdocs.org/sdr/08FDEA01458.md): Floor Support · corroded · Apr 19, 2008 · N498FE · Boeing 727232 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CORRODED AT BS 344, LBL 30 REMOVED CORROSION ON FLOOR SUPPORT STA 344, LBL 30, REF SRM 51-10- 6 PG 12. MATERIAL LOSS 50 PERCENT. FOUND TO BE OUT OF LIMITS, REF SRM 53-10-1 PG 1-3. FABRICATED NEW FLOOR SUPPORT AND SHIM, REF BOEING DWG 65-9617
- [SDR 08FDEA01457](https://openairdocs.org/sdr/08FDEA01457.md): Stringer Clip · cracked · Apr 19, 2008 · N498FE · Boeing 727232 · Fuselage Main, Attach Fittings
  > AFT PIT BILGE BODY FRAME, STR CLIP IS BUCKLED/CRACKED, BS 970, STR 27L. REMOVED AND REPLACED STRINGER CLIP AT BS 970, STRINGER 27L. IAW SRM 51-30-2, SRM 51-30-5. THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 08FDEA01452](https://openairdocs.org/sdr/08FDEA01452.md): Bracket · cracked · Apr 18, 2008 · N498FE · Boeing 727232 · Fuselage Main, Attach Fittings
  > E/E COMPARTMENT LEFT SIDE E1-1 RACK, SHELF FOR POWER SUPPLY TRANSFER RECTIFIER UNIT CRACKED AT FOWARD INBOARD SIDE. REMOVED MOUNTING SHELF, REMOVED DAMAGED BRACKET, FABRICATED NEW BRACKET, TREATED AND PRIMED AND INSTALLED BRACKET, RE SECURED E1-1 SHELF. REF
- [SDR 08FDEA01449](https://openairdocs.org/sdr/08FDEA01449.md): Attach Bracket · cracked · Apr 17, 2008 · N498FE · Boeing 727232 · Fuselage Main, Attach Fittings
  > MAIN ENTRY DOOR 1-L, S/N 261, UPPER AFT LINER ATTACH BRACKET IS CRACKED REMOVED BRACKET IN REF TO SRM 51-30-2 PG 2, VERIFIED MAT'L AS 2024 T3.040" IN REF TO DWG 65-49652-5 FABRICATED NEW ANGLE IN REF TO DWG 65-49652-5. TREATED AND PRIMED ANGLE IN REF TO SRM
- [SDR 08FDEA01448](https://openairdocs.org/sdr/08FDEA01448.md): Shear Tie · corroded · Apr 17, 2008 · N498FE · Boeing 727232 · Fuselage Internal Mounting Structure
  > FWD PIT SHEAR TIE CORRODED, STA 660 BETWEEN STR 27R - 26R REMOVED CORROSION ON FWD SHEAR TIE STA 660 STR 27R - 26R REF SRM 51-10-6 PG 12 ORIGINAL MATERIAL.050". MATERIAL REMAINING.035", MATERIAL LOSS.015". FOUND OUT OF LIMITS REF SRM 53-10-1 PG 1-2. FA
- [SDR 08FDEA01443](https://openairdocs.org/sdr/08FDEA01443.md): Stringer Clip · damaged · Apr 17, 2008 · N498FE · Boeing 727232 · Fuselage Main, Attach Fittings
  > STRINGER CLIP CRACKED ON STR 27L FS 950A REMOVED DAMAGED CLIP, REPLACED CLIP, REF SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR.
- [SDR 08FDEA01442](https://openairdocs.org/sdr/08FDEA01442.md): Panel · cracked · Apr 17, 2008 · N498FE · Boeing 727232 · Fuselage Miscellaneous Structure
  > LOWER PANEL 3456 RT IS CRACKED WITH ERODED AREA FLAME SPRAY. REPLACED CRACK AND FLAME SPRAY ON PANEL 3456 REF SRM 51-40-9 PARAGRAPHS 3D, 4E, 4F AND AMM 51-20-051-7. THIS IS CLASSIFIED AS A MINOR REPAIR.
- [SDR 08FDEA00341](https://openairdocs.org/sdr/08FDEA00341.md): Support · cracked · Feb 1, 2008 · N498FE · Boeing 727232 · Passenger/Crew Doors
  > FORWARD ENTRY DOOR LOWER AND UPPER AFT LATCH TORQUE TUBE SUPPORT CASTING HAS PARTIALLY DETACHED FROM DOOR FRAME AND FRAME IS CRACKED ON BOTH UPPER AND LOWER ATTACH POINTS. REMOVED AND REPLACED L1 FORWARD ENTRY DOOR PER 727-200 MM 52-11-001-4/ADJUSTMENT TEST G
- [SDR 07FDEA00205](https://openairdocs.org/sdr/07FDEA00205.md): Door · malfunctioned · Jan 26, 2007 · N498FE · Boeing 727232 · Passenger/Crew Doors
  > CREW ENTRY DOOR SHOWED CLOSED AND LOCKED WITH HANDLE FULL DOWN AND DOOR LIGHT OUT. AIRCRAFT WOULD NOT PRESSURIZE. RTB, UPON INITAL INSP FOUND ROLLERS ON AFT SIDE OF DOOR NOT IN TRACKS ON THE UPPER AND LOWER TRACK. UNABLE TO OPEN DOOR. AFTER OFF LOAD VISU
- [SDR 06FDEA0345](https://openairdocs.org/sdr/06FDEA0345.md): Repair · misinstalled · Jan 23, 2006 · N498FE · Boeing 727200 · Cargo/Baggage Doors
  > EXISTING REPAIR ON NR 3 CARGO DOORFWD TO AFT EDGE EXTERNAL SKIN DOES NOT COMPLY WITH EXISTING FAA DATA. REMOVED OLD DOUBLER AND DAMAGED SKIN IWA SRM 51-30-2 & 52-00-3 FIG3 INSTALLED REPAIR PARTS IAW SRM 51-30-2. REINSTALLED REMOVED FOR ACCESS IAW SRM 51-30-2
- [SDR 06FDEA0344](https://openairdocs.org/sdr/06FDEA0344.md): Skin · chafed · Jan 23, 2006 · N498FE · Boeing 727200 · Wing, Plate/Skin
  > RT WING FIXED TRAILING EDGE HAS CHAFE MARK AND SPOTS OF GOUGES FROM WS 224.5 TO WS 625.0 (SKIN UNDER FWD END OF SPOILER.) FABRICATED AND INSTALLED NEW STRAPS IAW SRM 57-30-2 REPLACEMENT PARTS FABRICATED ON TRAVELERS T5/564670,T5/564665,T5/564668,T5/564644,
- [SDR 06FDEA0343](https://openairdocs.org/sdr/06FDEA0343.md): Flange · worn · Jan 23, 2006 · N498FE · Boeing 727200 · Fuselage Main, Structure
  > AFT LWR. FUSELAGE FLANGE FOR NR 2 ENG LWR COWLING FWD EDGE CONTACT IS WORN. REMOVED AREA OF DAMAGE SRM51-10-01 &51-30-2.FABRICATED REPLACEMENT STRUCTURE P/N 65-23687-21 & SPLICE PARTS FABRICATED ON TRAVELER T5/565148. LOCATED DRILLED AND INSTALLED IAW SRM 51
- [SDR 06FDEA0273](https://openairdocs.org/sdr/06FDEA0273.md): Stringer · cracked · Jan 19, 2006 · N498FE · Boeing 727200 · Wing, Longeron/Stringer
  > LEFT WING STA 686.5 UPPER STRINGER 13 HAS A CRACK IN THE LOWER TAB SECTION THAT ATTACHES TO THE RIB PROTRUDING FROM UNDER RADIUS FILLER, REMOVE DAMAGE AND REPAIRS IAW BOEING S/B 727-57A159.
- [SDR 06FDEA0184](https://openairdocs.org/sdr/06FDEA0184.md): Repair · misinstalled · Jan 13, 2006 · N498FE · Boeing 727232 · Aircraft Structures
  > EXISTING REPAIRS 2 AT AFT AIR STAIR CUT OUT FWD CORNERS DO NOT COMPLY WITH FAA DATA. REMOVED RT AND LT REPAIR DOUBLERS IAW SRM 51-30-2. PERFORMED HFEC INSPECTION PER NTM-PT6 51-00-00 TO MARK THE END OF CRACKS. NO CRACKS NOTED BEYOND STOP DRILL. FABRICATED
- [SDR 06FDEA0146](https://openairdocs.org/sdr/06FDEA0146.md): Beam · corroded · Jan 11, 2006 · N498FE · Boeing 727200 · Fuselage Main, Structure
  > FOUND HORIZONTAL WALKWAY BEAM CHORD IS CORRODED AT STA 304 LEFT HAND SIDE OF NOSE LANDING GEAR WHEEL WELL. REMOVED WALKWAY BEAM IAW SRM 51-30-2, REMOVED FLOOR WEBS IAW SRM 51-30-2, REPLACED NEW WALKING BEAM CHORD IAW SRM 51-30-2, APPLIED LEVELING COMPOUND IAW
- [SDR 06FDEA0101](https://openairdocs.org/sdr/06FDEA0101.md): Stringer · misdrilled · Jan 9, 2006 · N498FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > FOUND MCD STRINGER 4L AT STA 450 HAS TOOLING MARKS AND 2 DRILLED MARKS ON OUTBD SIDE OF STRINGER, AFTER BLENDING AND FOUND OUT OF LIMITS PER SRM 5310-01, FIG 1, REMOVED AND REPLACED ALL DAMAGE PARTS IAW SRM 51-30-3.
- [SDR 06FDEA0086](https://openairdocs.org/sdr/06FDEA0086.md): Repair · unknown · Jan 8, 2006 · N498FE · Boeing 727232 · Aircraft Structures
  > FOUND PREVIOUSLY REPAIR INSTALLED AT STA 445, STR 17R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL THICKNESS AND TYPE, FASTENER NUMBER AND SPACING, GENERAL WORKMANSHIP AND REPAIR IS
- [SDR 06FDEA0085](https://openairdocs.org/sdr/06FDEA0085.md): Repair · unknown · Jan 8, 2006 · N498FE · Boeing 727232 · Aircraft Structures
  > FOUND PREVIOUSLY REPAIR INSTALLED AT STA 720, STR 23L WAS ACCOMPLISHED IAW SRM 53-30-3, FIG 1 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR IS
- [SDR 06FDEA0084](https://openairdocs.org/sdr/06FDEA0084.md): Repair · unknown · Jan 8, 2006 · N498FE · Boeing 727232 · Aircraft Structures
  > FOUND PREVIOUSLY REPAIR INSTALLED AT STA 720, STR 28R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG1, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR IS
- [SDR 06FDEA0083](https://openairdocs.org/sdr/06FDEA0083.md): Repair · unknown · Jan 8, 2006 · N498FE · Boeing 727232 · Aircraft Structures
  > FOUND PREVIOUSLY REPAIR INSTALLED AT STA 950E, STR 29R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 1 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR IS
- [SDR 06FDEA0082](https://openairdocs.org/sdr/06FDEA0082.md): Repair · unknown · Jan 8, 2006 · N498FE · Boeing 727232 · Aircraft Structures
  > FOUND PREVIOUSLY REPAIR INSTALLED AT STA 1130, STR 22L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 1 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR IS
- [SDR 06FDEA0081](https://openairdocs.org/sdr/06FDEA0081.md): Repair · unknown · Jan 8, 2006 · N498FE · Boeing 727232 · Aircraft Structures
  > FOUND PREVIOUSLY REPAIR INSTALLED ABOVE AIRSTAIRS CONTROL PANEL WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP
- [SDR 06FDEA0080](https://openairdocs.org/sdr/06FDEA0080.md): Repair · unknown · Jan 8, 2006 · N498FE · Boeing 727232 · Wing Structure
  > FOUND PREVIOUSLY 2 REPAIRS INSTALLED ON LT WING TIP LOWER SURFACE WAS ACCOMPLISHED IAW SRM 57-20-5 FIG 1, BASED ON EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENERS NUMBERS AND SPACING, GENERAL WORKMANSHIP A
- [SDR 06FDEA0079](https://openairdocs.org/sdr/06FDEA0079.md): Repair · unknown · Jan 8, 2006 · N498FE · Boeing 727232 · Wing Structure
  > FOUND PREVIOUSLY REPAIR INSTALLED AT UPPER SURFACE OF LT WING TIP WAS ACCOMPLISHED IAW SRM 57-20-1 FIG 2, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL TYPE AND THICKNESS, FASTENERS NUMBER AND SPACING, GENERAL WORKMANSH
- [SDR 06FDEA0078](https://openairdocs.org/sdr/06FDEA0078.md): Repair · unknown · Jan 8, 2006 · N498FE · Boeing 727232 · Aircraft Structures
  > FOUND PREVIOUSLY REPAIR INSTALLED AT STA 370, STR 24L WAS ACCOMPLISHED IAW SRM 53-30-3, FIG 4, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR I
- [SDR 06FDEA0077](https://openairdocs.org/sdr/06FDEA0077.md): Repair · unknown · Jan 8, 2006 · N498FE · Boeing 727232 · Aircraft Structures
  > FOUND PREVIOUSLY REPAIR INSTALLED AT STA 680, STR 27R WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 24, BASED ON AN EXTERNAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP AND REPAIR IS CLASS

Next page: https://openairdocs.org/deregistered/N498FE-2013-03-19/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 = 'N498FE' AND deregistration_id = 'N498FE-2013-03-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N498FE-2013-03-19/reports

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