# Service difficulty reports: Boeing 727-287

A list on [Boeing 727-287](https://openairdocs.org/model/boeing-727-287.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 54 reports

- [SDR GAIA03005OP](https://openairdocs.org/sdr/GAIA03005OP.md): Light · wrong part · Feb 5, 2003 · N916PG · Boeing 727287 · Emergency Lighting
  > DURING ROUTINE MAINTENANCE AT DFW, IT WAS DISCOVERED THAT THE L1 EMERGENCY EXIT LIGHT WOULD NOT TEST. FOUND INCORRECT UNIT INSTALLED. REMOVED AND REPLACED WITH CORRECT PART NR EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETU
- [SDR GAIA02133OP](https://openairdocs.org/sdr/GAIA02133OP.md): Warning Light · illuminated · Sep 19, 2002 · N916PG · Boeing 727287 · Engine Thrust Reverser
  > FLT 736 - BWI-CLT - AT TOP OF DESCENT, THE NR 2 ENGINE THRUST REVERSER LIGHT ILLUMINATED. THE NR 2 ENGINE THROTTLE WAS RETARDED, THE ENGINE WAS SHUTDOWN, AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT CONTINUED TO CLT AND LANDED WITHOUT FURTHER OCCURRENCE. THE
- [SDR GAIA02078OP](https://openairdocs.org/sdr/GAIA02078OP.md): Duct · broken · Jul 26, 2002 · N916PG · Boeing 727287 · Engine Anti-Icing System
  > FLT 863 - EWR-FWA - AT THE BEGINNING OF DESCENT TO FWA, THE NR 1 ENGINE FIRE WARNING CAME ON INTERMITTENTLY. POWER WAS REDUCED TO IDLE AND THE WARNING CEASED. THE AIRCRAFT CONTINUED TO FWA AND AN UNEVENTFUL LANDING WAS MADE. INSPECTION REVEALED THAT THE RIG
- [SDR GAIA02075OP](https://openairdocs.org/sdr/GAIA02075OP.md): Fire Loop · grounded · Jul 24, 2002 · N916PG · Boeing 727287 · Fire Detection
  > FLT 705 - DFW-FWA - AFTER TAKEOFF, THE FLIGHT CREW NOTICE THE NR 1 ENGINE FIRE LIGHT WAS ON INTERMITTENTLY. THE AIRCRAFT RETURNED TO DFW AND AN UNEVENTFUL LANDING WAS MADE. INSPECTION REVEALED THAT THE NR 1 ENGINE FIRE LOOP GROUNDING ON A MOUNTING BRACKET.
- [SDR GAIA02068OP](https://openairdocs.org/sdr/GAIA02068OP.md): Accessory Unit · inoperative · May 31, 2002 · N916PG · Boeing 727287 · Brake Anti-Skid Section
  > (LANDING GEAR ACCESSORY) SCHEDULED FLIGHT, DURING GEAR RETRACTION, THE PARKING BREAK ILLUINATED. CREW RECYCLED THE GEAR WITH ON CHANGE IN INDICATION. CREW DECLARED AN EMERGENCY LANDING. AT ABOUT 1000 FEET THE LIGHT EXTINGUISHED AND THE AIRCRAFT LANDING WE
- [SDR GAI2002F00001](https://openairdocs.org/sdr/GAI2002F00001.md): Accessory Unit · inoperative · May 31, 2002 · N916PG · Boeing 727287 · Brake Anti-Skid Section
  > (LANDING GEAR ACCESSORY) SCHEDULED FLIGHT, DURING GEAR RETRACTION, PARKING BRAKE LIGHT ILLUMINATED. CREW RECYCLED THE GEAR WITH NO CHANGE IN INDICATION. CREW DECLARED AN EMERGENCY LANDING. AT ABOUT 1000 FEET THE LIGHT EXTINGUISHED AND THE AIRCRAFT LANDING
- [SDR GAIA02010OP](https://openairdocs.org/sdr/GAIA02010OP.md): Skin · damaged · Feb 4, 2002 · N916PG · Boeing 727287 · Fuselage Main, Plate/Skin
  > DURING POST FLIGHT INSPECTION MAINTENANCE, FOUND DAMAGE TO THE FUSELAGE SKIN LOCATED AT STATION 610, STRINGER 19L WL 208. MAINTENANCE REMOVED DAMAGED AREA, AND REPAIRED PER DRAWING P52-R01. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M)
- [SDR GAIA01003OP](https://openairdocs.org/sdr/GAIA01003OP.md): Control Unit · malfunctioned · Jan 4, 2001 · N916PG · Boeing 727287 · Flight Control System
  > FLT 1735 - BNA-FWA - THE CREW REPORTED THAT THE AIRPLANE VIBRATES AND TE CONTROL WHEEL HARD TO TURN AS IF MAYBE A FLIGHT CONTROL IS OUT OF ADJUSTMENT. IT TAKES TWO UNITS OF RUDDER TRIM TO STRAIGHTEN THE PLANE IN LEVEL FLIGHT. THE AIRCRAFT MADE A SAFE LANDING
- [SDR GAIA00385](https://openairdocs.org/sdr/GAIA00385.md): Panel · shorted · Jul 10, 2000 · N916PG · Boeing 727287 · Crew Oxygen System
  > FLT 2015 - BIL-DEN - DURING CLIMB, SMOKE FROM THE FIRST OBSERVERS OXYGEN REGULATOR WAS NOTED. CREW RETURNED TO BIL AND MADE A SAFE LANDING WITHOUT ANY FURTHER INCIDENTS. MAINTENANCE INSPECTED AND FOUND BURNED SPOT ON OXYGEN REGULATOR LIGHT PANEL. PROBABLE S
- [SDR GAIA99209](https://openairdocs.org/sdr/GAIA99209.md): Structure · damaged · Nov 23, 1999 · N916PG · Boeing 727287 · Fuselage Main, Structure
  > AIRCRAFT FELL FROM JACKS. INSPECTED AND REPAIRS ACCOMPLISHED PER AVITAS REPAIR ORDER 99AVHM.059R0-1, REV A 8110-3 DTD 11/21/99 N/R 2998. (X)
- [SDR GAIA99208](https://openairdocs.org/sdr/GAIA99208.md): Trunnion · corroded · Nov 23, 1999 · N916PG · Boeing 727287 · Landing Gear Retraction/Extension System
  > RIGHT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTINGS INSIDE FACES ARE CORRODED. ACCOMPLISHED REPAIR TO LEFT AND RIGHT LANDING GEAR FORWARD TRUNNION REAR SPAR ATTACH FITTINGS IAW BOEING TELEX PSS-MIA-99-00007H. 8110-3 DATED 9/3/99 ISSUED. REF: N/R'S 74
- [SDR GAIA99207](https://openairdocs.org/sdr/GAIA99207.md): Hinge · loose · Nov 23, 1999 · N916PG · Boeing 727287 · Landing Gear Doors
  > RIGHT MAIN LANDING GEAR WING DOOR HAS PLAY AT THE FORWARD HINGE. ACCOMPLISHED REPAIR, RIGHT MAIN LANDING GEAR DOOR FRONT SPAR HINGE CLEVIS IAW BOEING TELEX PSS-MIA-99-00005H. 8110-3 DATED 8-3-99 ISSUED. REF: N/R 7344. (X)
- [SDR GAIA99206](https://openairdocs.org/sdr/GAIA99206.md): Keel Beam · cracked · Nov 23, 1999 · N916PG · Boeing 727287 · Fuselage Main, Keel
  > RIGHT WW BS 870.00 RBL ZERO KEEL BEAM AREA DENTED AND CRACKED. ACCOMPLISHED KEEL BEAM CHORD REPAIR AT STA 870 IAW AVITAS ENGINEERING REPAIR ORDER 99AVH.086R0-1, REV IR. 8110-3 DATED 10-21-99 ISSUED. REF: N/R 3071. (X)
- [SDR GAIA99205](https://openairdocs.org/sdr/GAIA99205.md): Skin · gouged · Nov 23, 1999 · N916PG · Boeing 727287 · Wing, Plate/Skin
  > RIGHT WING L/E UPPER SURFACE EXTERIOR SKIN HAS OLD GOUGE (PAINTED) OVER NR 6 L/E SLAT INBOARD TRACK. INSTALLED DOUBLER REPAIR AT RIGHT WING LEADING EDGE UPPER SURFACE EXTERIOR SKIN. REPAIR ACCOMPLISHED IAW SRM 57-30-4 FIG 4. REF: N/R 2364 AND 2365. (X)
- [SDR GAIA99204](https://openairdocs.org/sdr/GAIA99204.md): Lug · worn · Nov 23, 1999 · N916PG · Boeing 727287 · Leading Edge Devices
  > NR 2 L/E FLAP INBOARD BULLNOSE BEARING LUG WORN TOO LARGE FOR BEARING INSTALLATION AND LUG CORRODED AND PITTED. ACCOMPLIHSHED NR 2 LEADING EDGE FLAP BULLNOSE REPAIR IAW BOEING TELEX KHC-MIA-99-00003H, DATED 9-7-99. 8110-3 DATED 9-14-99 ISSUED. REF: N/R 188
- [SDR GAIA99203](https://openairdocs.org/sdr/GAIA99203.md): Bushing · damaged · Nov 23, 1999 · N916PG · Boeing 727287 · Trailing Edge Flaps
  > LEFT OUTBOARD FLAP OUTBOARD MECHANISM FOR AFT FLAG SEGMENT DRUM SUPPORT QUADRANT BUSHING HOLES ELONGATED. ACCOMPLISHED LEFT OUTBOARD MIDFLAP DRUM SUPPORT BUSHING REPAIR IAW AVITAS ENGINEERING REPAIR ORDER 99AVHM.084R0-1 REV IR. 8110-3 DATED 9-26-99 ISSUED. R
- [SDR GAIA99202](https://openairdocs.org/sdr/GAIA99202.md): Tube · chafed · Nov 23, 1999 · N916PG · Boeing 727287 · Wing Miscellaneous Structure
  > LEFT WING NR 1 TANK, VENT TUBE IS CHAFED ON LOWER SIDE. LOCATED ON TOP OF WING RIB AT WS 601.50. ACCOMPLISHED LEFT WING VENT LINE CHAFING REPAIR AT STA 601.5 IAW WITH AVITAS ENGINEERING REPAIR ORDER 99AVHM.052R0-1 RIV IR. 8110-3 DATED 7-22-99 ISSUED. REF:
- [SDR GAIA99201](https://openairdocs.org/sdr/GAIA99201.md): Housing · cracked · Nov 23, 1999 · N916PG · Boeing 727287 · Exterior Lighting
  > LEFT WING TIP LOGO LIGHT HOUSING CRACK ON INBOARD SIDE. ACCOMPLISHED LEFT WING TIP LOGO LIGHT HOUSING CRACK REPAIR IAW AVITAS ENGINEERING REPAIR ORDER 99AVHM,049R0-1 REV 1R. 8110-3 DATED 7-20-99 ISSUED. REF: N/R 1879. (X)
- [SDR GAIA99200](https://openairdocs.org/sdr/GAIA99200.md): Rib · damaged · Nov 23, 1999 · N916PG · Boeing 727287 · Wing, Rib/Bulkhead
  > RIGHT WING DAMAGED AT RIB LOWER FLANGE STA 686.5 AND STR 6. REPLACED FLANGE AT LOWER RIGHT WING RIB, STA 686.5, STR 6 IAW SRM 51-30-2. REF: N/R 2448. (X)
- [SDR GAIA99199](https://openairdocs.org/sdr/GAIA99199.md): Skin · dented · Nov 23, 1999 · N916PG · Boeing 727287 · Fuselage Main, Plate/Skin
  > SEVERAL DENTS PUSHED OUT OF SKIN AT BS 1342 AFT SKIN PANEL BETWEEN STR 16R AND STR 26R. INSTALLED DOUBLER REPAIR AT BS 1342 AFT SKIN PANEL BETWEEN STR 16 AND STR 26 RIGHT. REPAIR ACCOMPLISHED IAW SRM 53-30-3 FIG 2. REF: N/R 3573. (X)
- [SDR GAIA99198](https://openairdocs.org/sdr/GAIA99198.md): Skin · dented · Nov 23, 1999 · N916PG · Boeing 727287 · Fuselage Main, Plate/Skin
  > DENT AT BS 1342 AFT SKIN JUST BELOW STR 15 RIGHT. INSTALLED DOUBLER REPAIR AT BS 1342 AFT SKIN JUST BELOW STR 14 RIGHT. REPAIR ACCOMPLISHED IAW SRM 53-30-3 FIG 2. REF: N/R 3572. (X)
- [SDR GAIA99197](https://openairdocs.org/sdr/GAIA99197.md): Torque Box · cracked · Nov 23, 1999 · N916PG · Boeing 727287 · Passenger/Crew Doors
  > MAIN ENTRY DOOR AFT FRAME CORNER TORQUE BOX EIVDENCE OF CRACK AT LOWER AFT CORNER. REPLACED SECTION OF WEB AT MAIN DOOR LOWER AFT FRAME CORNER TORQUE BOX. REPAIR ACCOMPLISHED IAW SRM 51-40-2, FIG 1. REF: N/R 3924. (X)
- [SDR GAIA99196](https://openairdocs.org/sdr/GAIA99196.md): Skin · cracked · Nov 23, 1999 · N916PG · Boeing 727287 · Fuselage Main, Plate/Skin
  > COCKPIT EXTERIOR, NR 1 WINDOW CUT OUT HAS CRACK AT OUTBOARD UPPER CORNER. VERIFIED BY NDT. INSTALLED DOUBLER REPAIR AT COCKPIT EXTERIOR, NR 1 WINDOW CUT-OUT OUTBOARD UPPER CORNER. REPAIR ACCOMPLISHED IAW SRM 53-30-3 FIG 8. REF: N/R 3725. (X)
- [SDR GAIA99195](https://openairdocs.org/sdr/GAIA99195.md): Seat Track · worn · Nov 23, 1999 · N916PG · Boeing 727287 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT BS 1080 APPROXIMATELY LBL 45 LOCKING HOLES WORN. REPLACED SECTION OF CABIN SEAT TRACK FROM BS 960 TO BS 180, LBL 45. REPAIRED IAW SRM 53-10-5 FIG 7. REF: N/R 5326. (X)
- [SDR GAIA99194](https://openairdocs.org/sdr/GAIA99194.md): Spar · cracked · Nov 23, 1999 · N916PG · Boeing 727287 · Wing Spar
  > RIGHT WING BETWEEN WS 464 AND WS 491 BELOW NR 11 SPOILER LOWER AFT SPAR CHORD CRACK. INSTALLED REPAIR BETWEEN RIGHT WS 464 AND WS 491 BELOW NR 11 SPOILER AT THE LOWER AFT SPAR CHORD. REPAIR ACCOMPLISHED IAW BOEING TELEX KHC-MIA-99-0002H, 8110-3 DATED OCTOBER
- [SDR GAIA99193](https://openairdocs.org/sdr/GAIA99193.md): Skin · dented · Nov 23, 1999 · N916PG · Boeing 727287 · Ailerons
  > RIGHT, OUTBOARD AILERON LOWER SKIN DENTED AT TWO LOCATIONS. INSTALLED DOUBLER REPAIR AT RIGHT OUTBOARD AILERON LOWER SKIN. REPAIR ACCOMPLISHED IAW SRM 57-50-5 FIG 1. REF: N/R 3121. (X)
- [SDR GAIA99192](https://openairdocs.org/sdr/GAIA99192.md): Stringer · corroded · Nov 23, 1999 · N916PG · Boeing 727287 · Fuselage Main, Longeron/Stringer
  > E/E COMPARTMENT, RIGHT SIDE. CORROSION AT STR 25R BETWEEN STA 351 - STA 360, FORWARD APH POWER SUPPLY. INSTALLED STRINGER REPAIR BETWEEN STA 351 AND STA 360 AT STR 25 RIGHT. REPAIR ACCOMPLISHED IAW SRM 53-10-3 FIG 1. REF: N/R 3947. (X)
- [SDR GAIA99191](https://openairdocs.org/sdr/GAIA99191.md): Skin · damaged · Nov 23, 1999 · N916PG · Boeing 727287 · Fuselage Main, Plate/Skin
  > 10 INCH HOLE IN RIGHT SIDE FUSELAGE, STA 1015 TO STA 1025, STR 26 RIGHT. INSTALLED FUSELAGE EXTERIOR SKIN REPAIR FROM STA 1015 TO STA 1025, STR 26 RIGHT. REPAIR ACCOMPLISHED IAW SRM 53-30-3 FIG 1. REF: N/R 3036. (X)
- [SDR GAIA99190](https://openairdocs.org/sdr/GAIA99190.md): Stringer · damaged · Nov 23, 1999 · N916PG · Boeing 727287 · Fuselage Main, Longeron/Stringer
  > AFT CARGO, STR 26 RIGHT DAMAGED, STA 1020. INSTALLED REPAIR AT AFT CARGO COMPARTMENT STR 26 RT, STA 1020. REPAIR ACCOMPLISHED IAW SRM 53-10-3 FIG 1. REF: N/R 3038. (X)
- [SDR GAIA99189](https://openairdocs.org/sdr/GAIA99189.md): Skin · dented · Nov 23, 1999 · N916PG · Boeing 727287 · Fuselage Main, Plate/Skin
  > DEEP SCRATCH AND DENT ON BODY SKIN LOCATED BETWEEN BS 203.8 AND BS 228.8, STR 19 LT AND 24 LT, 13 INCH BOTTOM LT. INSTALLED FUSELAGE SKIN REPAIR BETWEEN BS 203.8 AND BS 228.8 BETWEEN STR 19 LT AND STR 24 LT. REPAIR ACCOMPLISHED IAW SRM 53-30-3 FIG 15A. REF:
- [SDR GAIA99188](https://openairdocs.org/sdr/GAIA99188.md): Seat Track · mechanical damag · Nov 23, 1999 · N916PG · Boeing 727287 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK RBL 45.5 BETWEEN BS 910 AND BS 930. THREE LOCKING HOLES UPPER SURFACE WITH TOOL MARKINGS. REPLACED SECTION OF CABIN SEAT TRACK BETWEEN BS 870 AND BS 950, RBL 45.5. REPAIR ACCOMPLISHED IAW SRM 53-10-5 FIG 7. REF: N/R 3305. (X)
- [SDR GAIA99187](https://openairdocs.org/sdr/GAIA99187.md): Skin · dented · Nov 23, 1999 · N916PG · Boeing 727287 · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STABILIZER L/E HAS SKIN DENT, APPROXIMATELY 15 INCHES FROM INBOARD END. INSTALLED DOUBLER REPAIR AT LEFT HORIZONTAL STABILIZER LEADING EDGE. REPAIR ACCOMPLISHED IAW SRM 55-10-3 FIG 1. REF: N/R 4315. (X)
- [SDR GAIA99186](https://openairdocs.org/sdr/GAIA99186.md): Skin · dented · Nov 23, 1999 · N916PG · Boeing 727287 · Fuselage Main, Plate/Skin
  > FUSELAGE LEFT SIDE EXTERIOR SKIN HAS TEMPORARILY FILLED DENT, STA 387, STR 18 LT. INSTALLED DOUBLER REPAIR AT FUSELAGE LEFT SIDE EXTERIOR SKIN STA 387, STR 18 LT. REPAIR ACCOMPLISHED IAW SRM 53-30-3 FIG 1. REF: N/R 3347. (X)
- [SDR GAIA99185](https://openairdocs.org/sdr/GAIA99185.md): Frame · cracked · Nov 23, 1999 · N916PG · Boeing 727287 · Fuselage Main, Frame
  > FS 930 LOWER FRAME IS CRACKED AT STR 14 LT. VERIFIED BY NDT INSPECTION. INSTALLED REPAIR AT FS 930, LOWER FRAME AT STR 14 LT. REPAIR ACCOMPLISHED IAW SRM 53-10-4 FIG 1. REF: N/R 5095. (X)
- [SDR GAIA99184](https://openairdocs.org/sdr/GAIA99184.md): Stringer · cracked · Nov 23, 1999 · N916PG · Boeing 727287 · Wing, Longeron/Stringer
  > RIGHT UPPER STR 10 CRACKED AT RIB STA 656.5. INSTALLED ANGLE REPAIR AT RIGHT WING UPPER STR 10 AT RIB STA 656.5. REPAIR ACCOMPLISHED IAW SB 727-57-0159. REF: N/R 2449. (X)
- [SDR GAIA99183](https://openairdocs.org/sdr/GAIA99183.md): Frame · cracked · Nov 23, 1999 · N916PG · Boeing 727287 · Fuselage Main, Frame
  > CABIN CIRCUMFERENTIAL TRACK AT BS 312 BELOW STR 13. INSTALLED REPAIR AT BS 312 BELOW STR 13 RIGHT CABIN CIRCUMFERENTIAL. REPAIR WAS ACCOMPLISHED IAW SRM 53-10-4 DETAIL 1. REF: N/R 3921. (X)
- [SDR GAIA99182](https://openairdocs.org/sdr/GAIA99182.md): Floor Beam · corroded · Nov 23, 1999 · N916PG · Boeing 727287 · Fuselage Main, Floor Beam
  > CABIN FLOOR BEAM BS 400 FROM LBL 12 TO RBL 24 EVIDENCE OF CORROSION AT UPPER SECTION. INSTALLED CABIN FLOOR BEAM REPAIR AT BS 400, FROM LBL 12 TO RBL 64. REPAIR ACCOMPLISHED IAW SRM 53-10-8 PAGE 21. REF: N/R 3933. (X)
- [SDR GAIA99181](https://openairdocs.org/sdr/GAIA99181.md): Rib · cracked · Nov 23, 1999 · N916PG · Boeing 727287 · Leading Edge Devices
  > NR 2 L/E SLAT INBOARD TRACK OUTBOARD MOUNT RIB IS CRACKED AT UPPER FLANGE BEINDING RADIUS APPROXIMATELY 1.50 INCHES AFT FROM SLAT FRONT SPARE. INSTALLED REPAIR AT THE NR 2 LEADING EDGE SLAT INBOARD TRACK OUTBOARD MOUNT RIB UPPER FLANGE. REPAIR ACCOMPLISHED I
- [SDR GAIA99180](https://openairdocs.org/sdr/GAIA99180.md): Floor Beam · corroded · Nov 23, 1999 · N916PG · Boeing 727287 · Fuselage Main, Floor Beam
  > FLOOR BEAM AT BS 1070 ACCESS THROUGH AFT BAGGAGE COMPARTMENT. UPPER FLANGE LOWER SECTION AT APPROXIMATELY LBL 70.5 HAS EVIDENCE OF CORROSION. REPLACED SECTION OF FLOOR BEAM FROM BLR 39 TO BLR 70.5 AT BS 1070. REPAIR ACCOMPLISHED IAW SRM 53-10-8 FIG 3. REF:
- [SDR GAIA99179](https://openairdocs.org/sdr/GAIA99179.md): Shear Plate · corroded · Nov 23, 1999 · N916PG · Boeing 727287 · Fuselage Miscellaneous Structure
  > LEFT AFT LAVATORY FLOOR - MANY AREAS OF CORROSION AND CORROSION ON ALL WALL SUPPORT ANGLES. REPLACED SECTION OF SHEAR PLATE FROM BS 1130 TO BS 1176, FROM LBL 15 TO LBL 68.5. REPAIR ACCOMPLISHED IAW SRM 51-10-1 PARA 4 AND SRM 51-30-2. REPLACED SECTION OF SEA
- [SDR GAIA99178](https://openairdocs.org/sdr/GAIA99178.md): Skin · damaged · Nov 23, 1999 · N916PG · Boeing 727287 · Fuselage Main, Plate/Skin
  > CHECK INTEGRITY OF FLUSH MP PATCH REPAIR PREVIOUSLY MADE AT BS 400 BETWEEN STR 21R AND STR 22R. REPLACED FLUSH REPAIR AT BS 400 BETWEEN STR 21R AND STR 22R. REPAIR ACCOMPLISHED IAW SRM 53-30-2 FIG 2. REF: N/R 3585 FOR DETAILS. (X)
- [SDR GAIA99177](https://openairdocs.org/sdr/GAIA99177.md): Carriage · cracked · Nov 23, 1999 · N916PG · Boeing 727287 · Trailing Edge Flaps
  > LEFT WING INBOARD FLAP. MID-FLAP NR 11 RIB LOCATED BY NR 4 FLAP. CARRIAGE COMPARTMENT HAS A CRACK. INSTALLED CARRIAGE DOUBLER REPAIR AT LT WING INBOARD FLAP, MID-FLAP NR 11 RIB LOCATED BY THE NR 4 FLAP CARRIAGE. REPAIR ACCOMPLISHED IAW SRM 57-50-4 FIG 2.
- [SDR GAIA99176](https://openairdocs.org/sdr/GAIA99176.md): Skin · dented · Nov 23, 1999 · N916PG · Boeing 727287 · Fuselage Main, Plate/Skin
  > SKIN DENTS AT BS 211.8 AND BS 219.80 JUST LWR OF LWR RT PITOT TUBE. INSTALLED DOUBLER REPAIR AT BS 219.8 EXTERIOR FUSELAGE SKIN JUST LWR OF THE LWR RT PITOT TUBE. MATERIAL USED 2024-T3, 0-.050 INCH, 9 INCH BY 9 INCH. REPAIR ACCOMPLISHED IAW SRM 53-30-3 FIG
- [SDR GAIA99175](https://openairdocs.org/sdr/GAIA99175.md): Skin · dented · Nov 23, 1999 · N916PG · Boeing 727287 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED LOCATED BETWEEN BS 380 AND BS 400 JUST BELOW STR 19R. INSTALLED FUSELAGE SKIN DOUBLER REPAIR BETWEEN BS 380 AND BS 400 JUST BELOW STR 19R. REPAIR ACCOMPLISHED IAW SRM 53-30-3 FIG 1. REF: N/R 3582. (X)
- [SDR GAIA99174](https://openairdocs.org/sdr/GAIA99174.md): Skin · misrepaired · Nov 23, 1999 · N916PG · Boeing 727287 · Fuselage Main, Plate/Skin
  > CHECKED INTEGRITY OF FLUSH REPAIR PREVIOUSLY MADE AT BS 1070 STR 24R AND STR 25R. INSTALLED FLUSH REPAIR AT BS 1070 BETWEEN STR 25R AND STR 24R. REPAIRED ACCOMPLISHED IAW SRM 53-30-3 FIG 2. REF: AIRBOURNE N/R 3586. (X)
- [SDR 97ZZZX3357](https://openairdocs.org/sdr/97ZZZX3357.md): Floor Beam · corroded · Jun 1, 1997 · N920PG · Boeing 727287 · Fuselage Main, Floor Beam
  > DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON FLOOR BEAM LOWER CHORD AT FS 1130.
- [SDR 97ZZZX3356](https://openairdocs.org/sdr/97ZZZX3356.md): Skin · gouged · Jun 1, 1997 · N920PG · Boeing 727287 · Fuselage Main, Plate/Skin
  > DURING C-CHECK INSPECTION, SEVERAL GOUGES WERE NOTED ON AIRCRAFT SKIN PANEL AT FS 1070L AT S18L.
- [SDR 97ZZZX3355](https://openairdocs.org/sdr/97ZZZX3355.md): Stringer · corroded · Jun 1, 1997 · N920PG · Boeing 727287 · Fuselage Main, Longeron/Stringer
  > DURING C-CHECK INSPECTION, LEVEL 2 CORROSION WAS NOTED ON S29R AT FS 1166.
- [SDR 97ZZZX2949](https://openairdocs.org/sdr/97ZZZX2949.md): Hinge Cavity · corroded · Jun 1, 1997 · N920PG · Boeing 727287 · Passenger/Crew Doors
  > DURING C-CHECK INSPECTION, LEVEL 2 CORROSION WAS NOTED ON INSIDE OF UPPER HINGE CAVITY.
- [SDR 97ZZZX2948](https://openairdocs.org/sdr/97ZZZX2948.md): Frame Cap · corroded · Jun 1, 1997 · N920PG · Boeing 727287 · Fuselage Main, Frame
  > DURING C-CHECK INSPECTION, LEVEL 2 CORROSION WAS NOTED ON 1183 BULKHEAD FRAME CAP RT SIDE AT S17R.

Next page: https://openairdocs.org/model/boeing-727-287/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 aircraft_model_key = '727287'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-287/reports

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