# Service difficulty reports: N277FE, cancelled Aug 10, 2015

A list on [N277FE, cancelled Aug 10, 2015](https://openairdocs.org/deregistered/N277FE-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 2 · 71 reports

- [SDR FDEA201101180222](https://openairdocs.org/sdr/FDEA201101180222.md): Controller · failed · Jan 18, 2011 · N277FE · Boeing 727233 · Cabin Pressure Controller
  > DURING CRUISE FLIGHT THE ALTITUDE WARNING HORN SOUNDED. THE CABIN ALTITUDE WAS APPROACHING 11,000 FT & RISING. RAN THE QRH & CHECKED THE PANEL WHICH OFFERED NO RELIEF, THEN IAW THE QRH. WE DESCENDED TO 10,000'. SELECTED THE STANDBY MODE. STILL NO RELIEF.
- [SDR FDEA200901110124](https://openairdocs.org/sdr/FDEA200901110124.md): Stringer · corroded · Jan 11, 2009 · N277FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > CORROSION AT ATTACHING RIVET HEADS STA 950-1010 STR 27L IN AFT PIT. FOUND CORROSION OUT OF LIMITS IAW SRM 53-10-1. REMOVED STRINGER 27L FROM BS 950A TO BS 1010 IAW SRM 51-30-2. FABRICATED NEW STRINGER AND SPLICES IAW SRM 53-10-3. INSTALLED REPAIR PARTS IAW
- [SDR FDEA200901110123](https://openairdocs.org/sdr/FDEA200901110123.md): Stringer · corroded · Jan 11, 2009 · N277FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > CORROSION AT ATTACHING RIVET HEADS STA 1010-1090 STR 27L IN AFT PIT. FOUND CORROSION OUT OF LIMITS IAW SRM 53-10-1, REMOVED STRINGER 27L FROM BS 1010 TO BS 1090 IAW SRM 51-30-2. FABRICATED NEW STRINGER AND SPLICES IAW SRM 53-10-3. INSTALLED REPAIR PARTS I
- [SDR FDEA200901070064](https://openairdocs.org/sdr/FDEA200901070064.md): Stringer · corroded · Jan 7, 2009 · N277FE · Boeing 727233 · Fuselage Main, Structure
  > FWD CARGO PIT, CORROSION INSIDE CHANNEL STRINGER 23R AT STA. 720E - 720F. REMOVED ACCESS PANEL 3440 IAW SRM 51-30-2. CUT-OUT DAMAGE STR 23R BETWEEN STA 720E TO 740 IAW SRM 53-10-3 FIG 1 DETAIL I. FABRICATED REPAIR FILLER AND 2 EA SPLICES IAW SRM 53-10-3 FI
- [SDR FDEA200901050042](https://openairdocs.org/sdr/FDEA200901050042.md): Stringer · corroded · Jan 5, 2009 · N277FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > FWD CARGO CORROSION AT STR 27R AND STA 620 INSIDE THE STRINGER CHANNEL. REMOVED CORROSION IAW SRM 51-10-2 AND UT AREA IAW NDTM 51-00-00 FIG 2 PART 4. FOUND TO BE OUT-OF-LIMITS IAW SRM 53-10-1 FIG 1. REMOVED RIBS AT STA. 606 & 612, AND STRINGER TIES IAW SRM
- [SDR FDEA200901050041](https://openairdocs.org/sdr/FDEA200901050041.md): Spar · cracked · Jan 5, 2009 · N277FE · Boeing 727200 · Wing Spar
  > RT WING T/E, FALSE SPAR INBD ATTACHMENT HAS LOOSE HARDWARE AND SEPARATION BETWEEN PARTS, WBL 118 FOUND CRACKED. REPAIR ACCOMPLISHED PER DRAWING SR27-57-038 REV "C". STD. REWORK DRAWING INBD BEAM CRACK REPAIR.
- [SDR FDEA200901030009](https://openairdocs.org/sdr/FDEA200901030009.md): Skin · cracked · Jan 3, 2009 · N277FE · Boeing 727233 · Leading Edge Devices
  > NR 6 SLAT HAS A BROKEN BOLT AT INBD HOOK AT AFT MOUNT AND BROKEN RIVET AND HAS CRACK INDICATIONS. HFEC VERIFIED 4 CRACKS ALL TERMINATE AT FASTENER HOLES OR SKIN EDGE. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-50-3 AND 51-30-2.
- [SDR FDEA200901030008](https://openairdocs.org/sdr/FDEA200901030008.md): Skin · cracked · Jan 3, 2009 · N277FE · Boeing 727233 · Leading Edge Devices
  > NR 6 SLAT HAS A CRACK AT OTBD HOOK AFT OF MOUNT BOLT. HFEC VERIFIED CRACK TERMINATES AT FASTENER HOLE. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-50-3 AND SRM 51-30-2.
- [SDR FDEA200812245290](https://openairdocs.org/sdr/FDEA200812245290.md): Web · cracked · Dec 24, 2008 · N277FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIR, RT LWR TORQUE BOX INBD VERTICAL WEB IS CRACKED AT 02 PLACES AT LIGHTING HOLE STA 1218. REMOVED AFT AIRSTAIRS FLOOR PANEL AND ANGLE FOR ACCESS IAW SRM 51-30-2. CUTOUT DAMAGED AREA IAW SRM 51-40-2 FIG 1. FABRICATED REPAIR PARTS FROM 2024T3, 0.032
- [SDR FDEA200812245288](https://openairdocs.org/sdr/FDEA200812245288.md): Skin · damaged · Dec 24, 2008 · N277FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > FUSELAGE, FASTENER INSTALLED AT SEAM AT STA 550, STR 21L REMOVED SUBJECT FASTENER AND TRIMMED OUT DAMAGED AREA IAW EA NR 7-5330-126879. REPAIRED IAW EA NR 7-5330-126879, FUSELAGE, PLATES AND SKIN AD 98-11-03 R1 MCD CUTOUT PLATING REPAIR AT STA 554.
- [SDR FDEA200812245284](https://openairdocs.org/sdr/FDEA200812245284.md): Skin · dented · Dec 24, 2008 · N277FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > GOUGE AND DENT ON FUSELAGE SKIN STA 1030, STR 28L. FOUND GOUGE OUT OF LIMIT IAW B727 SRM 53-30-1 FIG 1 AND 2. CUTOUT DAMAGED AREA IAW B727 SRM 53-30-3 FIG 3. FABRICATED DOUBLER FROM 2024T3, 0.071 AND A FILLER FROM 2024T3, 0.063 INCH IAW B727 SRM 53-30-3 FIG
- [SDR FDEA200812245282](https://openairdocs.org/sdr/FDEA200812245282.md): Stringer · corroded · Dec 24, 2008 · N277FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > FWD CARGO HAS CORROSION AT STRINGER 28R AND STA 680 ON STRINGER CHANNEL UNDER LEVELING COMPOUND. REMOVED STRINGER SPLICE IAW SRM 51-30-2. FABRICATED NEW STR SPLICE IAW SRM 53-10-2FIG 9 AND 53-10-3 FIG 1. TREATED AND PRIMED AND INSTALLED NEW SPLICE AT FWD CA
- [SDR FDEA200812245281](https://openairdocs.org/sdr/FDEA200812245281.md): Shear Tie · damaged · Dec 24, 2008 · N277FE · Boeing 727233 · Fuselage Internal Mounting Structure
  > MISDRILLED STRINGER SHEAR TIE AT 9G BULKHEAD AND STR 12R REMOVED STR SHEAR TIE ON 9G BULKHEAD, STR12R IAW SRM 51-30-2. FABRICATED PART OF STRINGER TIE FROM 2024T3, 0.032 AND FRAME REPAIR PART FROM 7075O AND HEAT TREATED TO 7075T6 IAW SRM 51-20-1, 51-10-3 AN
- [SDR FDEA200812245279](https://openairdocs.org/sdr/FDEA200812245279.md): Skin · dented · Dec 24, 2008 · N277FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > EXT FUSELAGE, SKIN DENTED AT STA 700 STR 24L FOUND DENT OUT OF LIMITS IAW SRM 53-30-1 FIG 1. CUTOUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-10-2 FIG. 1 AND 53-30-2 FIG 2. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR PA
- [SDR FDEA200812245278](https://openairdocs.org/sdr/FDEA200812245278.md): Channel · corroded · Dec 24, 2008 · N277FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > FWD CARGO CORROSION AT STR 27R AND STA 680 ON STRINGER CHANNEL REMOVED CORRODED CHANNEL IAW SRM 51-30-2. FABRICATED NEW CHANNEL IAW SRM 51-10-2. INSTALLED NEW CHANNEL AT FWD CARGO STRINGER 27R, STA 680 IAW SRM 51-30-2
- [SDR FDEA200812245277](https://openairdocs.org/sdr/FDEA200812245277.md): Strap · corroded · Dec 24, 2008 · N277FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > FWD CARGO BAY CORROSION AT AFT OF STA 680, STR 26R TO STR 26L REPAIRED (REMOVED & REPLACED) TEAR STRAP AT FWD PIT STA 680 BETWEEN STR 26R AND 26L IAW DRAWING 65-56238 REV. B AND SRM 51-30-2.
- [SDR FDEA200812245276](https://openairdocs.org/sdr/FDEA200812245276.md): Hinge · cracked · Dec 24, 2008 · N277FE · Boeing 727233 · Fuselage, Door Hinge
  > EXTERIOR FUSELAGE AFT SEGMENT OF MCD HINGE, FUE SIDE, HAS A LOBE CRACKED STA. 680-720 REMOVED AFT SECTION MAIN CARGO DOOR HINGE IAW SRM 51-30-2. FABRICATED NEW HINGE IAW SRM 51-30-5 AND 51-10-1. TREATED AND PRIMED NEW HINGE IAW SRM 51-10-2. INSTALLED NEW M
- [SDR FDEA200812245275](https://openairdocs.org/sdr/FDEA200812245275.md): Stringer Clip · damaged · Dec 24, 2008 · N277FE · Boeing 727233 · Fuselage Main, Attach Fittings
  > MISDRILLED STRINGER CLIP AT 9G BULKEAD, STR 4R REMOVED STRINGER CLIP ON 9G BULKHEAD STR 4R IAW SRM 51-30-2. CUTOUT DAMAGED AREA IAW SRM 53-10-4. FABRICATED PARTS OF STRINGER CLIP IAW SRM 51-20-1 AND 51-10-3. FABRICATED FRAME REPAIR PARTS AND HEAT TREATED IAW
- [SDR FDEA200812245274](https://openairdocs.org/sdr/FDEA200812245274.md): Skin · dented · Dec 24, 2008 · N277FE · Boeing 727233 · Elevator, Plate/Skin
  > GOUGE AND DENT IN UPPER SURFACE SKIN OF LT ELEVATOR, O/B END OF CONTROL TAB CUTOUT, AT JOINT OF ELEVATOR T/E WEDGES. BLENDED AND SMOOTHED GOUGE AREA IAW SRM 51-10-1. FABRICATED REPAIR DOUBLERS IAW SRM 55-20-3. TREATED AND PRIMED PART IAW SRM 51-10-2. INSTA
- [SDR FDEA200812245273](https://openairdocs.org/sdr/FDEA200812245273.md): Web · cracked · Dec 24, 2008 · N277FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIRS LT LOWER TORQUE BOX I/B VERTICAL WEB IS CRACKED AT UPPER ROW OF RIVETS BETWEEN STA 1203 AND STA. 1223 REMOVED PANEL AT AFT AIRSTAIRS LT VERTICAL WEB FOR ACCESS IAW SRM 51-30- 2. CUTOUT DAMAGED AREA IAW SRM 51-40-2 FIG 1. FABRICATED REPAIR PART
- [SDR FDEA200812245270](https://openairdocs.org/sdr/FDEA200812245270.md): Web · cracked · Dec 24, 2008 · N277FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIRS, RH LOWER TORQUE BOX I/B VERTICAL WEB IS CRACKED AT UPPER ROW OF RIVETS BETWEEN STA. 1203 AND STA 1223 REMOVED PANEL AT AFT AIRSTAIRS RH VERTICAL WEB FOR ACCESS IAW SRM 51-30-2 CUTOUT DAMAGED AREA IAW SRM 51-40-2 FIG 1. FABRICATED REPAIR PART A
- [SDR FDEA200812245269](https://openairdocs.org/sdr/FDEA200812245269.md): Web · cracked · Dec 24, 2008 · N277FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > AFT AIRSTAIRS, LT TORQUE BOX I/B VERTICAL WEB IS CRACKED AT BS.1225, WB 190 APROX REMOVED AFT AIRSTAIRS FLOOR PANEL AND ANGLE FOR ACCESS IAW SRM 51-30-2. CUTOUT DAMAGED AREA IAW SRM 51-40-2 FIG 1. FABRICATED REPAIR PART AND FILLER IAW SRM 53-10-2 FIG 6 AN
- [SDR FDEA200812195243](https://openairdocs.org/sdr/FDEA200812195243.md): Skin · bulged · Dec 19, 2008 · N277FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > EXTERIOR FUSELAGE SKIN BULGE SAT 185, STR 24L CUTOUT DAMAGED AREA IAW SRM 53-30-3 FIG 14. FABRICATED REPAIR PART AND DOUBLER IAW SRM 53-30-3 FIG 14. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 53-30-3 AND 51-30-2.
- [SDR FDEA200812195244](https://openairdocs.org/sdr/FDEA200812195244.md): Frame · corroded · Dec 19, 2008 · N277FE · Boeing 727233 · Fuselage Main, Frame
  > CORROSION ON FRAME REPAIR 1070 AND 27L REMOVED PREVIOUS REPAIR IAW SRM 51-30-2. FABRICATE REPAIR PART, IAW SRM 53-10-2 FIG 5, AND 54-40-3 FIG 1. HEAT TREATED IAW ER 2-37153-801 REV A. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED NEW FRAME REPAIR IAW SRM 5
- [SDR FDEA200812185225](https://openairdocs.org/sdr/FDEA200812185225.md): Skin · dented · Dec 18, 2008 · N277FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > DENT STA 720D, STR 18L. CUT OUT DAMAGED AREA DIM (1 7/8" X 7/8") IAW SRM 53-10-3 FIG 2. REMOVED FLOORBOARDS ROW "A" STA 720A TO 740 IAW SRM 51-30-2. FABRICATE REPAIR PARTS DOUBLER AND FILLER IAW SRM 53-30-2 FIG 2 AND 53-30-3 FIG 2. TREATED AND PRIMED IAW SRM 5
- [SDR FDEA200812165183](https://openairdocs.org/sdr/FDEA200812165183.md): Web · cracked · Dec 16, 2008 · N277FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > AFT AIR STAIRS, LT LOWER TORQUE BOX INBD VERTICAL WEB IS CRACKED AT LIGHTNING HOLE BETWEEN STA 1263-1283. TRIMMED OUT DAMAGED AREA IAW SRM 51-40-2, FIG 1. FABRICATE REPAIR IAW SRM 51-40 -2 FIG 1, AND 53-10-2 FIG 6. TREATED AND PRIMED IAW SRM 51-10-2. INSTALL
- [SDR 07FDEA02527](https://openairdocs.org/sdr/07FDEA02527.md): Duct · leaking · Jul 19, 2007 · N277FE · Boeing 727233 · Pneumatic Distribution System
  > NR 1 ENGINE STRUT OVERHEAT LIGHT CAME ON AT 6000' DURING CLIMB, RAN QRH PROCEDURE AND WERE ABLE TO MAKE THE LIGHT GO OUT WITH REDUCING POWER. ADVANCING POWER CAUSED THE LIGHT TO COME ON AGAIN. REDUCED NR 1 ENGINE TO IDLE POWER AND RETURN TO MEMPHIS. MEM R
- [SDR 06FDEA2539](https://openairdocs.org/sdr/06FDEA2539.md): Floorbeam · corroded · Jul 11, 2006 · N277FE · Boeing 727200 · Fuselage Main, Floor Beam
  > FLOORBEAM CAP CORRODED FS 1110 AT LBL 67 MAIN CABIN. REMOVED DAMAGE, FABRICATED, ALODINED, PRIMED AND INSTALLED FLOORBEAM CAP REPAIR ALL IAW FX B727-200 SRM 53-10-1 FIG 4A, 53-10-8 FIG 3, 51-10-2, 51-30-2.
- [SDR 06FDEA2538](https://openairdocs.org/sdr/06FDEA2538.md): Stringer · corroded · Jul 11, 2006 · N277FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > FWD PIT STR 27L HAS CORROSION AT STA 740. REMOVED DAMAGE, FABRICATED, ALODINED, PRIMED AND INSTALLED STRINGER REPAIR IAW FX B727-200 SRM 53-10-1, 53-10-3 FIG 1, 51-10-6, 51-30-2 AND 51-10-2.
- [SDR 06FDEA2537](https://openairdocs.org/sdr/06FDEA2537.md): Stringer · corroded · Jul 11, 2006 · N277FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > FWD LOWER CARGO COMPT S28L SPLICE CORRODED AT FS 680. REMOVED DAMAGE, FABRICATED, ALODINED, PRIMED AND INSTALLED STRINGER REPAIR ALL IAW FX B727-200 SRM 53-10-1, 53-0-3 FIG 4, 53-10-3 FIG 1, 51-10-6, 51-10-2 AND 51-30-2.
- [SDR 06FDEA2536](https://openairdocs.org/sdr/06FDEA2536.md): Skin · corroded · Jul 11, 2006 · N277FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > FWD LOWER CARGO AT STA 535 BETWEEN STR 28L AND STR 28R SKIN HAS CORROSION AROUND ANTENNA CUTOUT. REMOVED DAMAGE, FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR TO FUSELAGE SKIN IAW FX B727-200 SRM 53-30-1, 53-30-2 FIG 2, 53-30-3 FIG 1, 51-10-2 AND 51-30-2.
- [SDR 06FDEA2535](https://openairdocs.org/sdr/06FDEA2535.md): Skin · gouged · Jul 11, 2006 · N277FE · Boeing 727200 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN GOUGED STA 1300 LT ABOVE AIR STAIR CUTOUT. REMOVED DAMAGE, FABRICATED, ALODINED, PRIMED AND INSTALLED. REPAIR ALL IAW B727-200 SRM 53-30-1, 53-30-2 FIG 3, 53-30-3 FIG 1, 51-10-2.
- [SDR 05FDEA02381](https://openairdocs.org/sdr/05FDEA02381.md): Motor · malfunctioned · Aug 10, 2005 · N277FE · Boeing 727233 · Trailing Edge Flap Control System
  > O/B T/E FLAPS WOULD NOT POSITION WITH FLAP HANDLE. FLT CREW C/W QRH PROCEDURES AND HAVE A C/B PULLED. INSPECTED O/B FLAPS FOR POSSIBLE JAM AND NONE NOTED. WITH HYD ON, THE O/B FLAP CONTROL VALVE IS BYPASSING FLUID. REMOVED AND REPLACED O/B FLAP HYD MOTOR
- [SDR 04FDEA00084](https://openairdocs.org/sdr/04FDEA00084.md): Frame · damaged · Jan 8, 2004 · N277FE · Boeing 727200 · Fuselage Main, Frame
  > SCREW DAMAGE IN FRAME AT BS 1110 STR 26. *S/D* FOUND SCREW DAMAGE ON FRAME TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED DAMAGE AREA AND FABRICATED REPAIR DOUBLER FROM 7075-70.071 LOT 491543, APPLIED PROTECTIVE TREATMENT AND INSTALLED REPAIR DOUBLER. ALL
- [SDR 04FDEA00083](https://openairdocs.org/sdr/04FDEA00083.md): Frame · damaged · Jan 8, 2004 · N277FE · Boeing 727200 · Fuselage Main, Frame
  > SCREW DAMAGE ON FRAME AT BS 1070 STR 26L WL 148. *S/D* DAMAGE ON FRAME AT BS 1070 STR 26L WL 148 OUT OF LIMITS. REMOVED DAMAGE AND REPAIRED PER FED EX EA 7-5310-55191 AND SRM 51-40-3, 51-10-2.
- [SDR 04FDEA00082](https://openairdocs.org/sdr/04FDEA00082.md): Frame · damaged · Jan 8, 2004 · N277FE · Boeing 727200 · Fuselage Main, Frame
  > SCREW DAMAGE ON FRAME BS 1090 STR 26L WL 148. *S/D* FOUND SCREW DAMAGE ON FRAME TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED DAMAGED AREA AND FABRICATED REPAIR DOUBLER FROM 7075-0.071, HEAT TREATED TO T6 AND INSTALLED PER SRM 51-40-3, 51-10-2, 51-30-2.
- [SDR 04FDEA00004](https://openairdocs.org/sdr/04FDEA00004.md): Frame · cracked · Jan 2, 2004 · N277FE · Boeing 727200 · Fuselage Main, Frame
  > WHILE WORKING CARD NR N00298, FOUND DENTED AND CRACKED FRAME AT BS 640 RBL 13 WL 152. FOUND CRACK IN 640 FRAME OUT OF LIMITS. REPAIRED PER FED EX EA 7-5330-70609, SRM 53-10-1.
- [SDR 03FDEA02323](https://openairdocs.org/sdr/03FDEA02323.md): Stringer · corroded · Dec 29, 2003 · N277FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > CORROSION IN FWD CARGO BAY ON STR 27L BS 550-560. FOUND CORROSION ON STR 27L BS 550 TO 560 TO PENETRATE 100 PERCENT OF ORIGINAL.040 THICKNESS. CUT AND REMOVED STRINGER BS 549 TO BS 567 AND INSTALLED REPAIR MADE FROM BAC 1498-132 LOT 507364 AND BAC 1498-
- [SDR 03FDEA02324](https://openairdocs.org/sdr/03FDEA02324.md): Stringer · corroded · Dec 29, 2003 · N277FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 28L AND SPLICE AT BS 676 FWD CARGO BAY. CORROSION FOUND TO BE OUT OF LIMITS ON STRINGER, STRINGER SPLICE, SKIN AND SHEAR TIE. REPAIRED DAMAGED STRINGER AND STRINGER SPLICE PER SRM 53-10-2, 53-10-3. REPAIRED SKIN PER SRM 53-30-3 AND
- [SDR 03FDEA02322](https://openairdocs.org/sdr/03FDEA02322.md): Shear Tie · corroded · Dec 29, 2003 · N277FE · Boeing 727200 · Fuselage Main, Structure
  > CORROSION AT SHEAR TIE BS 950F LBL 9, COMMON TO STR 29 LT. REMOVED CORROSION FROM SHEAR TIE 1 X2 X.009 INCHES FROM ORIGINAL OF.071. OUT OF LIMITS PER SRM 53-10-1. CUT OF SHEAR TIE AT BS 950F, LBL 9, COMMON TO STR 29 LT. AND REPAIRED FRAME IAW SRM 53-10-4
- [SDR 03FDEA02321](https://openairdocs.org/sdr/03FDEA02321.md): Stringer · corroded · Dec 29, 2003 · N277FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
  > CORROSION AT STRINGER 29 LT, BS 970-990. BLENDED OUT CORROSION AT STRINGER 29 LT BS 970-990 AND INSTALLED REPAIR STRAP PER SR 27-53-023.
- [SDR 02FDEA00225](https://openairdocs.org/sdr/02FDEA00225.md): Fire Detector · malfunctioned · Mar 29, 2002 · N277FE · Boeing 727233 · Fire Detection
  > NR 1 STRUT OVERHEAT LIGHT CAME ON. REMOVED AND REPLACED FIRE DETECTION UNIT PER SMP 20-10-017, 28-14-011-5, 28-14-001-2.
- [SDR 01FDEA001003](https://openairdocs.org/sdr/01FDEA001003.md): Connector · loose · Nov 18, 2001 · N277FE · Boeing 727233 · Landing Gear System Wiring
  > DURING DESCENT NR 1 ENG STRUT LIGHT ILLUM. REMOVED AND REPLACED GEAR PINS AND SECURED LOOSE CONNECTOR. OK FOR SERVICE.
- [SDR 01FDEA00734](https://openairdocs.org/sdr/01FDEA00734.md): Stringer · corroded · Aug 10, 2001 · N277FE · Boeing 727233 · Fuselage Main, Structure
  > N 549 STR 29L CORRODED FROM BS 950E-950F. R&R STRINGER PER SRM 51-40-4, 51-30-2.
- [SDR 01FDEA00733](https://openairdocs.org/sdr/01FDEA00733.md): Floorbeam · corroded · Aug 10, 2001 · N277FE · Boeing 727233 · Fuselage Main, Floor Beam
  > N 905 BS 1030 FUSELAGE FLOORBEAM CORRODED BETWEEN NR 3 & 4 SEAT TRACKS. R&R FLOORBEAM PER SRM 53-10-8.
- [SDR 01FDEA00732](https://openairdocs.org/sdr/01FDEA00732.md): Intercostal · corroded · Aug 10, 2001 · N277FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > N 907 INTERCOSTAL BETWEEN #3 & 4 MAIN CABIN SEAT TRACK BS 1040 CORRODED. R&R INTERCOSTAL PER SRM 53-10-1.
- [SDR 01FDEA00731](https://openairdocs.org/sdr/01FDEA00731.md): Fitting · corroded · Aug 10, 2001 · N277FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > N 960 NOSE LAND GEAR FWD FITTING CORRODED. R&R FITTING PER SRM 51-30-2.
- [SDR 01FDEA00730](https://openairdocs.org/sdr/01FDEA00730.md): Seat Track · corroded · Aug 10, 2001 · N277FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > N 915 #5 MAIN CABIN SEAT TRACK CORRODED BETWEEN BS 1050-1070. R&R SEAT TRACK PER SRM 53-10-5.
- [SDR 01FDEA00729](https://openairdocs.org/sdr/01FDEA00729.md): Bushing · corroded · Aug 10, 2001 · N277FE · Boeing 727233 · Wing Main, Frame Structure
  > N 970 LH FWD TERMINAL PIN BUSHING CORRODED. R&R BUSHING PER 57-41-011-4.
- [SDR 01FDEA00728](https://openairdocs.org/sdr/01FDEA00728.md): Bushing · corroded · Aug 10, 2001 · N277FE · Boeing 727233 · Wing Main, Frame Structure
  > N 971 RH FWD TERMINAL PIN BUSHING CORRODED. R&R BUSHING PER IAW 57-41-011-4.

Next page: https://openairdocs.org/deregistered/N277FE-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 = 'N277FE' AND deregistration_id = 'N277FE-2015-08-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N277FE-2015-08-10/reports

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