# Service difficulty reports: N222FE, cancelled Apr 25, 2013 A list on [N222FE, cancelled Apr 25, 2013](https://openairdocs.org/deregistered/N222FE-2013-04-25.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 3 · 112 reports - [SDR FDEA200812245268](https://openairdocs.org/sdr/FDEA200812245268.md): Indicator · failed · Dec 24, 2008 · N222FE · Boeing 727233 · Trailing Flap Position Indicating System > ASSYMETRIC OUTBOARD TRAILING EDGE FLAPS DURING FLAP RETRACTION FROM FLAPS 2 TO FLAPS 0. REMOVED AND REPLACED OUTBOARD FLAP POSITION INDICATOR AND PERFORMED OPERATIONAL CHECK IAW AMM 27-52-021-2 ALL CHECK GOOD. OK FOR SERVICE. R/I FROM FACT PREMATURE REMO - [SDR 07FDEA00103](https://openairdocs.org/sdr/07FDEA00103.md): Unknown · malfunctioned · Jan 16, 2007 · N222FE · Boeing 727233 · Central Warning > UPON RAISING GEAR HANDLE THE FOLLOWING LIGHTS ILLUMINATED, CAPT AND FO DECISION HEIGHT, SPEED BRAKE DO NOT ARM, SPEED BRAKE ARMED, ALL REVERSER OPERATING, RED AND GREEN GEAR AND DOOR LIGHTS, TAIL SKID, GREEN AND AMBER LE FLAPS, FO ALT. - [SDR 06FDEA04127](https://openairdocs.org/sdr/06FDEA04127.md): Flap System · malfunctioned · Nov 28, 2006 · N222FE · Boeing 727233 · Trailing Edge Flap Control System > DURING FLAP RETRACTION AFTER TAKEOFF OUTBOARD TRAILING EDGE FLAPS WENT ASYMETRIC AND LOCKED OUT AT 2 DEGREES. FOLLOWED QRH PROCEDURES. LANDING UNEVENTFUL. REMOVED AND REPLACED INDICATOR PER M/M 27-52-000-0 SYSTEM OPS CHECKS OK AT THIS TIME. PREMATURE REMOV - [SDR 06FDEA03746](https://openairdocs.org/sdr/06FDEA03746.md): Skin · cracked · Oct 20, 2006 · N222FE · Boeing 727233 · Fuselage Main, Plate/Skin > MAIN ENTRY DOOR EXT SKIN AFT UPPER CORNER HAS 2 CRACKS. REPAIRED MAIN ENTRY DOOR AFT UPPER DOOR IAW SRM 52-00-. FABRICATED REPAIR DOUBLER FROM 2024 T-3.063 C BATCH 986936, FILLER FROM 2024 T-3.050C BATCH 1136567 TREATED AND PRIMED IAW SRM 51-10-2. INSTA - [SDR 06FDEA03632](https://openairdocs.org/sdr/06FDEA03632.md): Frame · cracked · Oct 13, 2006 · N222FE · Boeing 727233 · Fuselage Main, Frame > FRAME AT BS 1352 INNER STRUCTURE CRACKED AT 8:00 POSITION FOUND UPON REMOVAL OF OUTER CHORD. REPAIRED INNER STRUCTURE ON FRAME STA 1352 IAW SRM 51-40-3. - [SDR 06FDEA03449](https://openairdocs.org/sdr/06FDEA03449.md): Shim · corroded · Sep 27, 2006 · N222FE · Boeing 727233 · Trailing Edge Flaps > LT NR2 FLAP TRACK AFT MOUNT TAPERED SHIM CORRODED REMOVED CORROSION FOUND OUT OF LIMITS REMOVED.035 FROM ORG MAT.045 REMAINING MAT.010 IAW SRM 57-10-6 AND 57-10-1 FIG 1 FABERICATED NEW SHIM ON MAE TRAVLER T6/ 631803. - [SDR 06FDEA03448](https://openairdocs.org/sdr/06FDEA03448.md): Shim · corroded · Sep 27, 2006 · N222FE · Boeing 727233 · Trailing Edge Flaps > LT NR 3 FLAP TRACK BEAM CENTER MOUNT TAPERED SHIM CORRODED REMOVED CORROSION FOUND OUT OF LIMITS, CORROSION EXFOLIATION IAW SRM 51-10-6 AND SRM57-10-1 FIG 1 DETAIL 1. FABRICATED NEW SHIM ON MAE TRAVLER T6/31804. - [SDR 06FDEA03440](https://openairdocs.org/sdr/06FDEA03440.md): Flap Track · corroded · Sep 26, 2006 · N222FE · Boeing 727233 · Trailing Edge Flaps > LT NR 3 FLAP TRACK BEAM FWD MOUNT SUPPORT FITTING CORRODED. REMOVED AND REPLACED BUSHNG IAW SR 27-57-020 AND SOPM 20-50-03. REMOVED CORROSION FROM FITTING ORIGINAL MATERIAL.750 AFTER REWORK.740. FOUND TO BE WITHIN LIMITS IAW SRM 51-106 AND SR 27-51-020 TRE - [SDR 05FDEA03006](https://openairdocs.org/sdr/05FDEA03006.md): Display · inoperative · Sep 20, 2005 · N222FE · Boeing 727233 · Weather Radar System > AFTER T/O, SWITCHING FROM TERRAIN TO WX MODE OR RADAR, LOST RANGE MARKER AND DATA DISPLAY. ACTUAL WX RETURNS WORKED. REMOVED AND REPLACED INDICATOR R/T AS PRECAUTIONARY. REF B727-200MM SEC 34-41-031-4 AND 34-41-041-4. - [SDR 05FDEA02717](https://openairdocs.org/sdr/05FDEA02717.md): Tube · chafed · Aug 30, 2005 · N222FE · Boeing 727233 · Hydraulic System, Main > HYD SYS A FAILED (W/FLAPS 15) WHILE CONFIGURING TO LAND AT MEM. REPLACED ENGINES NR 1 AND 2 ENGINE DRIVEN HYDRAULIC PUMPS, REF MM29-11-041-2. REPLACED BOTH CASE DRAIN FILTERS. REPLACED SYSTEM "A" HYDRAULIC RETURN FILTER, R/I. REMOVED AND REPLACED SYSTEM A - [SDR 05FDEA00318](https://openairdocs.org/sdr/05FDEA00318.md): Module · failed · Feb 26, 2005 · N222FE · Boeing 727233 · Landing Gear Position and Warning > WHEN GEAR HANDLE IS UP, RIGHT GEAR SAFE GREEN LIGHT WILL NOT TEST. REPLACED BULBS CYCLED CBS. SWAPPED RIGHT GEAR AND LEFT GEAR LIGHTS IN LEFT POSITION, RIGHT LIGHT WORKED IN RIGHT POSITION, LEFT LIGHT DID NOT WORK. CK'D CONTINUITY THROUGH WARN LIGHT PUSH TO - [SDR 04FDEA03105](https://openairdocs.org/sdr/04FDEA03105.md): Actuator · malfunctioned · Nov 11, 2004 · N222FE · Boeing 727233 · Landing Gear Retraction/Extension System > NOSE GEAR WOULD NOT EXTEND DURING APPROACH. RED NOSE LIGHT ILLUMINATED. UPON LEVEL OFF IE UNLOADING, THE A/C NOSE GEAR EXTENDED, NORMAL LANDING. REMOVED AND REPLACED NOSE LANDING GEAR DOWN LOCK ACT, IAW B727-200MM 32-33-011-4, ACFT STILL REQUIRES JACKING FO - [SDR 04FDEA01742](https://openairdocs.org/sdr/04FDEA01742.md): Floorbeam · corroded · Jun 15, 2004 · N222FE · Boeing 727200 · Fuselage Main, Floor Beam > CORROSION ON FLOORBEAM, STA 760, LBL 66, WL 206. *S/D* CORROSION OUT OF LIMITS. REMOVED STUB FLOORBEAM BS 760 LT SIDE. DRILLED UP & INSTALLED NEW STUB FLOORBEAM WL 200 PER SRM 51-30-2, 51-30-5, 53-10-1. - [SDR 04FDEA01741](https://openairdocs.org/sdr/04FDEA01741.md): Frame · cracked · Jun 15, 2004 · N222FE · Boeing 727200 · Fuselage Main, Frame > FOUND FRAME BS 783 RT FASTENER HOLE CRACKED. REPAIR PER EO 7-5310-7-3367 PART 9. REPAIRED FRAME BS 783 RT PER EO 7-5310-7-3367 PART 9. - [SDR 04FDEA01631](https://openairdocs.org/sdr/04FDEA01631.md): Frame · dented · Jun 7, 2004 · N222FE · Boeing 727200 · Fuselage Main, Frame > FWD CARGO BAY STA 680 FRAME DENTED STR 25 LT. - [SDR 04FDEA01630](https://openairdocs.org/sdr/04FDEA01630.md): Floorbeam · corroded · Jun 7, 2004 · N222FE · Boeing 727200 · Fuselage Main, Floor Beam > CORROSION ON FLOORBEAM STRAP AT BS 950, LBL 9, WL 138. - [SDR 04FDEA01629](https://openairdocs.org/sdr/04FDEA01629.md): Floorbeam · corroded · Jun 7, 2004 · N222FE · Boeing 727200 · Fuselage Main, Floor Beam > CORROSION ON FLOORBEAM AT BS 950, RBL 27.5, WL 208 UPPER FLANGE. - [SDR 04FDEA01619](https://openairdocs.org/sdr/04FDEA01619.md): Structure · corroded · Jun 4, 2004 · N222FE · Boeing 727200 · Fuel Storage > CORROSION AT LOWER SURFACE OF CTR FUEL TANK, BS 830, RBL 26, WL 160, JUST ABOVE RT PRIMARY HEAT EXCHANGER. CORROSION AT LOWER SURFACE OF CENTER FUEL TANK - BS 830, RBL 26, WL 160 ABOVE PRIMARY HEAT EXCHANGERS FOUND TO BE OUT OF LIMITS PER SRM 57-30-1. REPAI - [SDR 04FDEA01605](https://openairdocs.org/sdr/04FDEA01605.md): Floorbeam · corroded · Jun 3, 2004 · N222FE · Boeing 727200 · Fuselage Main, Floor Beam > CORROSION ON FLOORBEAM AT BS 950 RBL 27.5 WL 208 UPPER FLANGE. REMOVED CORROSION ON FLOORBEAM IAW SRM 51-10-6 AND FED EX EA 7-5310-55308. - [SDR 04FDEA01604](https://openairdocs.org/sdr/04FDEA01604.md): Floorbeam · corroded · Jun 3, 2004 · N222FE · Boeing 727200 · Fuselage Main, Floor Beam > WHILE CLOSING MAIN CARGO FLOOR PANELS FOUND BS 1070, LBL 25 TO RBL 60, WL 200 LOWER FLOORBEAM FWD SIDE CORRODED. REPAIRED FLOOR BEAM BS 1070 PER FED EX EA 7-5310-55306. - [SDR 04FDEA01603](https://openairdocs.org/sdr/04FDEA01603.md): Frame · damaged · Jun 3, 2004 · N222FE · Boeing 727200 · Fuselage Main, Frame > BS 990 FRAME LT PREVIOUS REPAIR CRACKED ON BOTTOM. FOUND DAMAGE TO BS 990 FRAME, STR 24 LT TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED AREA PER SRM 51-40-3 AND FED EX EA 7-5310-55307. - [SDR 04FDEA01602](https://openairdocs.org/sdr/04FDEA01602.md): Frame · dented · Jun 3, 2004 · N222FE · Boeing 727200 · Fuselage Main, Frame > SIDE FRAME DENTED BS 460 RBL 65 STR 16R. FOUND DENT IN 460 FRAME, STR 16R TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED FRAME PER SRM 51-40-3 AND FED EX EA 7-5310-70665A. - [SDR 04FDEA01601](https://openairdocs.org/sdr/04FDEA01601.md): Floorbeam · corroded · Jun 3, 2004 · N222FE · Boeing 727200 · Fuselage Main, Floor Beam > CORROSION (C53-224-04) ON FLOORBEAM AROUND NUT PLATE HOLES BS 1130, LBL 27 - LBL 43, WL 207. CORROSION OUT OF LIMITS. REPAIRED 1130 FLOORBEAM UPPER CHORD LBL 27-43 WL 207 IAW SRM 53-10-8 FIG 10. - [SDR 04FDEA01566](https://openairdocs.org/sdr/04FDEA01566.md): Floorbeam · corroded · Jun 2, 2004 · N222FE · Boeing 727200 · Fuselage Main, Floor Beam > WHILE CLOSING MAIN CARGO FLOOR PANELS FOUND BS 970 LBL 12 WL 200 LOWER FLOORBEAM CORRODED. CORROSION OUT OF LIMITS. REMOVED CORRODED FLOORBEAM LOWER CHORD 1 X 4.25 INCHES. FABRICATED & INSTALLED REPAIR ANGLES (2 EA) & FILLER, AND RESTORED ALL ACCESS PER SRM - [SDR 04FDEA01565](https://openairdocs.org/sdr/04FDEA01565.md): Floorbeam · corroded · Jun 2, 2004 · N222FE · Boeing 727200 · Fuselage Main, Floor Beam > CORROSION (C53-224-01) FLOORBEAM UPPER FLANGE LWR SURFACE IS GOUGED AND CORROSION STA 400 LBL 2-8 WL 208. REPAIRED FLOORBEAM AT BS 400, LBL 2-8, WL 208 IAW SRM 53-10-8 FIG 3, 51-40-3, 51-10-3, FED EX MM 51-20-000-7, 51-20-021-7, SRM 51-30-2. ORIGINAL MATERIA - [SDR 04FDEA01564](https://openairdocs.org/sdr/04FDEA01564.md): Floorbeam · corroded · Jun 2, 2004 · N222FE · Boeing 727200 · Fuselage Main, Floor Beam > CORROSION (C53-224-01, 3) FLOORBEAM STA 1130 LWR CHORD FWD FLANGE UPPER SURFACES CORRODED LBL 1-45 WL 200 AROUND NUT PLATE. REMOVED CORROSION ON 1130 FLOORBEAM, LOWER CHORD, FWD FLANGE UPPER AND LOWER SURFACES LBL 1 - LBL 45, WL 200 AROUND FASTENER HOLES. OR - [SDR 04FDEA01563](https://openairdocs.org/sdr/04FDEA01563.md): Stringer Clip · cracked · Jun 2, 2004 · N222FE · Boeing 727200 · Fuselage Main, Attach Fittings > FWD CARGO COMPARTMENT STA 520 WL 150 RBL 21 STR 26R STRINGER CLIP CRACKED. REMOVED AND REPLACED STRINGER CLIP BS 520, WL 150, RBL 21, STR 26R. REMOVED DAMAGE 1 X 5 INCH FROM EDGE OF CLIP. ALODINED AND PRIMED BARE METAL IAW SRM 51-30-2, 51-10-01, 51-10-2. - [SDR 04FDEA01562](https://openairdocs.org/sdr/04FDEA01562.md): Frame · dented · Jun 2, 2004 · N222FE · Boeing 727200 · Fuselage Main, Frame > FWD CARGO COMPARTMENT STA 560 WL 155 LBL 35 FLOOR FRAME DENTED. CUT OUT DAMAGE IN FRAME AT BS STA 560 WL 155 LBL 35 AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-3 FIG 1. - [SDR 04FDEA01561](https://openairdocs.org/sdr/04FDEA01561.md): Failsafe · corroded · Jun 2, 2004 · N222FE · Boeing 727200 · Fuselage Main, Frame > CORROSION (C53-224-01, 2) ON FRAME, STA 760, RBL 70, WL 207. FOUND CORROSION ON FRAME FAIL SAFE STRAP AT BS 760 RBL 70, WL 207 TO BE OUT OF LIMITS PER SRM 53-10-2. REMOVED DAMAGED SECTION OF FAIL SAFE STRAP. FABRICATED REPAIR SECTION OF STRAP AND DOUBLER P - [SDR 04FDEA01499](https://openairdocs.org/sdr/04FDEA01499.md): Frame · dented · May 27, 2004 · N222FE · Boeing 727200 · Fuselage Main, Frame > FWD CARGO COMPARTMENT STA 520, WL 163, LBL 39 FRAME DENTED. REMOVED DAMAGE ON FRAME B.S. 520, WL 163, LBL 39 IN A 1 1/2 X 17 1/2 AREA. FABRICATED REPAIR DOUBLER USING 7075-T6.050 LOT 553781. ALODINED, PRIMED AND INSTALLED IAW 727 SRM 51-30-2, 51-40-3 SH3 A - [SDR 04FDEA01498](https://openairdocs.org/sdr/04FDEA01498.md): Floorbeam · corroded · May 27, 2004 · N222FE · Boeing 727200 · Fuselage Main, Floor Beam > CORROSION (C53-224-01,3) FLOORBEAM STA 1110 WL 208 CORRODED UPPER CHORD. REMOVED CORROSION FROM BS 1110 FLOOR BEAM, FOUND TO BE OUT OF LIMITS PER SRM 53- 10-1. ACCESSED AREA, REPLACED UPPER CHORD PER FED EX EA 7-5310-77727, RESTORED ACCESS PER SRM 51-30-2 A - [SDR 04FDEA01465](https://openairdocs.org/sdr/04FDEA01465.md): Stringer Clip · cracked · May 26, 2004 · N222FE · Boeing 727200 · Fuselage Main, Attach Fittings > CRACKED STRINGER CLIP, STA 950C, STRINGER 3L. REMOVED AND REPLACED STRINGER CLIP AT STA 950C, STR 3L IAW SRM 51-30-2. - [SDR 04FDEA01464](https://openairdocs.org/sdr/04FDEA01464.md): Frame · dented · May 26, 2004 · N222FE · Boeing 727200 · Fuselage Main, Frame > FRAME UPPER CHORD DENTED BS 1010, RBL 30 ABOVE STR 26R. CUT OUT DAMAGED AREA OF FRAME AT BS 1010, RBL 30 ABOVE STR 26R IN 1.75 X 1.5 DIAMETER AREA. FABRIATED TYPICAL FORMED SECTION REPAIR. ALODINED, PRIMERED AND INSTALLED IAW SRM 51-40-3 FIGURE 1, SRM 51-10- - [SDR 04FDEA01446](https://openairdocs.org/sdr/04FDEA01446.md): Stringer Clip · cracked · May 25, 2004 · N222FE · Boeing 727200 · Fuselage Main, Attach Fittings > STRINGER CLIP CRACKED STA 950B STRINGER 7R. REMOVED AND REPLACED STRINGER CLIP AT STA 950B, STR 7R IAW SRM 51-30-2. - [SDR 04FDEA01445](https://openairdocs.org/sdr/04FDEA01445.md): Frame · dented · May 25, 2004 · N222FE · Boeing 727200 · Fuselage Main, Frame > FWD CARGO COMPARTMENT STA 580, WL 155, LBL 35 FLOOR FRAME DENTED. FWD CARGO COMPARTMENT STA 580, WL 155, LBL 35 FRAME DENTED OUT OF LIMITS PER SRM 53-10-1. REPAIRED FRAME PER SRM 51-40-3 AND FED EX EA 7-5310-70665. - [SDR 04FDEA01444](https://openairdocs.org/sdr/04FDEA01444.md): Frame · dented · May 25, 2004 · N222FE · Boeing 727200 · Fuselage Main, Frame > STA 600 FRAME DENTED BETWEEN STR 24 LT & 25 LT IN FWD CARGO BAY. FRAME AT BS 600 BETWEEN STR 24 LT & 25 LT IN FWD CARGO BAY DENT FOUND OUT OF LIMITS PER SRM 53-10-1. REPAIR FRAME PER SRM 51-40-3 AND FED EX EA 7-5310-70665. - [SDR 04FDEA01443](https://openairdocs.org/sdr/04FDEA01443.md): Frame · dented · May 25, 2004 · N222FE · Boeing 727200 · Fuselage Main, Frame > FWD CARGO BAY STA 660 FRAME DENTED AT STR 24 LT. REPAIRED DENTED FRAME AT FWD CARGO BAY STA 660, STR 24L IAW EA 7-5310-70665 AND SRM 51-40-3. - [SDR 04FDEA01442](https://openairdocs.org/sdr/04FDEA01442.md): Frame · dented · May 25, 2004 · N222FE · Boeing 727200 · Fuselage Main, Frame > FWD CARGO STA 680 FRAME DENTED AT STR 24 RT. CUT OUT DAMAGE ON FRAME INNER CHORD BS 680, STR 24 RT. DRILLED UP REPAIR DOUBLER AND INSTALLED PER SRM 51-40-3 FIG 1 AND FED EX EA 7-5310-70665. - [SDR 04FDEA01435](https://openairdocs.org/sdr/04FDEA01435.md): Floorbeam · corroded · May 24, 2004 · N222FE · Boeing 727200 · Fuselage Main, Floor Beam > CORROSION (C53-224-01) ON FLOORBEAM UPPER SURFACE BS 380 RBL 25 TO 35 WL 208. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED AREA RBL 25.75 TO 27.75 AND RBL 46 TO 48 AT BS 380, WL 208. FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLERS, BOT - [SDR 04FDEA01434](https://openairdocs.org/sdr/04FDEA01434.md): Stringer Clip · cracked · May 24, 2004 · N222FE · Boeing 727200 · Fuselage Main, Attach Fittings > CRACKED STRINGER CLIP, STA 950D, STRINGER 6R. REMOVED AND REPLACED STRINGER CLIP AT BS 950D, STR 6R IAW SRM 51-30-2. - [SDR 04FDEA01433](https://openairdocs.org/sdr/04FDEA01433.md): Stringer Clip · cracked · May 24, 2004 · N222FE · Boeing 727200 · Fuselage Main, Attach Fittings > CRACKED STRINGER CLIP, STA 950C, STRINGER 5R. REMOVED AND REPLACED STRINGER CLIP AT STA 950C, STR 5R IAW SRM 51-30-2. - [SDR 04FDEA01432](https://openairdocs.org/sdr/04FDEA01432.md): Stringer Clip · cracked · May 24, 2004 · N222FE · Boeing 727200 · Fuselage Main, Attach Fittings > CRACKED STRINGER CLIP, STA 950C, STRINGER 3R. REMOVED AND REPLACED STRINGER CLIP AT STA 950C, STR 3R IAW SRM 51-30-2. - [SDR 04FDEA01428](https://openairdocs.org/sdr/04FDEA01428.md): Floorbeam · corroded · May 24, 2004 · N222FE · Boeing 727200 · Fuselage Main, Floor Beam > CORROSION (C53-224-01), ON FLOORBEAM LWR FLANGE STA 600 RBL 49 TO 60 WL 201. REMOVED CORROSION ON LOWER FLANGE FLOORBEAM CHORD AT BS 600, RBL 49-60, WL 201. FOUND TO BE OUT OF LIMITS. ACCESSED AREA AND CUT LOWER CHORD FROM RBL 35 TO END OF FLOORBEAM. FABRI - [SDR 04FDEA01427](https://openairdocs.org/sdr/04FDEA01427.md): Floorbeam · corroded · May 24, 2004 · N222FE · Boeing 727200 · Fuselage Main, Floor Beam > CORROSION (C53-224-01), ON FLOORBEAM BS 344 LBL 33 TO 60 WL 208 AROUND NUT PLATE HOLES. REMOVED CORROSION ON FLOORBEAM, BS 344. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 FIG 1. REMOVED AND REPLACED FLOORBEAM UPPER CHORD BS 344, RBL 65 - LBL 65, WL 208. ALL - [SDR 04FDEA01426](https://openairdocs.org/sdr/04FDEA01426.md): Frame · dented · May 24, 2004 · N222FE · Boeing 727200 · Fuselage Main, Frame > FWD CARGO STA 660 FRAME DENTED AT STR 24 RT. TRIMMED OUT DENT DAMAGE FROM FLANGE ON FRAME STA 660, STR 24R, LOCATED AND DRILLED FASTENER HOLES IN REPAIR DOUBLER PER SRM 51-40-3 PG 1-6 AND EA 7-5310-70665. ALODINED, PRIMERED AND INSTALLED FASTENERS PER SRM 51 - [SDR 04FDEA01425](https://openairdocs.org/sdr/04FDEA01425.md): Stringer Clip · cracked · May 24, 2004 · N222FE · Boeing 727200 · Fuselage Main, Attach Fittings > STRINGER CLIP CRACKED STA 950A STR 7R. REMOVED AND REPLACED STRINGER CLIP AT BS 950A, STR 7R IAW SRM 51-30-2. - [SDR 04FDEA01424](https://openairdocs.org/sdr/04FDEA01424.md): Stringer Clip · cracked · May 24, 2004 · N222FE · Boeing 727200 · Fuselage Main, Attach Fittings > STRINGER CLIP CRACKED STA 950C STR 7R. REMOVED AND REPLACED STRINGER CLIP AT BS 950C, STR 7R IAW SRM 51-30-2. - [SDR 04FDEA01423](https://openairdocs.org/sdr/04FDEA01423.md): Stringer Clip · cracked · May 24, 2004 · N222FE · Boeing 727200 · Fuselage Main, Longeron/Stringer > STRINGER CLIP CRACKED STA 950A STR 6R. REMOVED AND REPLACED STRINGER CLIP AT BS 950A, STR 6R IAW SRM 51-30-2. - [SDR 04FDEA01422](https://openairdocs.org/sdr/04FDEA01422.md): Floorbeam · corroded · May 24, 2004 · N222FE · Boeing 727200 · Fuselage Main, Floor Beam > FLOORBEAM TOP TEE CORRODED STA 1030 LBL 25 - RBL 25 WL 208. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPAIRED DAMGE AREA PER SRM 53-10-8. - [SDR 04FDEA01421](https://openairdocs.org/sdr/04FDEA01421.md): Stringer · corroded · May 24, 2004 · N222FE · Boeing 727200 · Fuselage Main, Longeron/Stringer > FWD CARGO STR 26 RT STA 720B CORRODED. REMOVED DAMAGE AREA OF STRINGER AND STIN AT BS 720B. FABRICATED AND INSTALLED REPAIRS IAW SRM 53-30-3, 53-10-3. Next page: https://openairdocs.org/deregistered/N222FE-2013-04-25/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 = 'N222FE' AND deregistration_id = 'N222FE-2013-04-25' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N222FE-2013-04-25/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.