# Service difficulty reports: Boeing 727-51C

A list on [Boeing 727-51C](https://openairdocs.org/model/boeing-727-51c.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 9 · 433 reports

- [SDR UPS03241647](https://openairdocs.org/sdr/UPS03241647.md): Warning Light · illuminated · Dec 9, 2003 · N905UP · Boeing 72751C · Engine Fuel Indicating System
  > NR 3 ENG FUEL FILTER WARNING LIGHT ILLUMINATED.
- [SDR UPS03241337](https://openairdocs.org/sdr/UPS03241337.md): Skin · lightning strike · Sep 24, 2003 · N903UP · Boeing 72751C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SP LT FUSELAGE SKIN JUST AFT OF MAIN CARGO DOOR AT SKIN LAP HAS A LIGHTNING STRIKE AT STA 620 BETWEEN STRINGER 13L AND 14L. BLENDED OUT LIGHTNING STRIKE AREA FOUND CRACKED. CUT OUT DAMAGE, NDT CUTOUT AREA NO CRACKS NOTED AT CUTOUT, FABRICATED
- [SDR UPS03241336](https://openairdocs.org/sdr/UPS03241336.md): Support Fitting · cracked · Sep 24, 2003 · N903UP · Boeing 72751C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SP RIGHT FUSELAGE TO WING SUPPORT FITTING IS CRACKED AT STA 760.95 AT RBL 70.5. REMOVED AND REPLACED FITTING IAW DWG 65C33202 AND SRM 51-30-02.
- [SDR UPS03241270](https://openairdocs.org/sdr/UPS03241270.md): Skin · cracked · Sep 24, 2003 · N903UP · Boeing 72751C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: SPV, LIGHTNING STRIKE AND AREA OF CORROSION 15 INCHES ABOVE NR 1 PYLON AT TR SECTION ON EXTERIOR FUSELAGE AT STA 1283 LONG 9L-10L. BLENDED OUT CORROSION AND LIGHTNING STRIKE, FOUND A CRACK AT BLEND OUT AREA, CUT OUT DAMAGE, NDT VERIFIED NO
- [SDR UPS03241123](https://openairdocs.org/sdr/UPS03241123.md): Battery · discharged · Aug 19, 2003 · N904UP · Boeing 72751C · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS BOTH NOT WORKING. REMOVED AND REPLACED BATTERIES. OPS CK GOOD.
- [SDR UPS03241013](https://openairdocs.org/sdr/UPS03241013.md): Indicator · malfunctioned · Jul 31, 2003 · N902UP · Boeing 72751C · Fire Detection
  > FIRE INDICATION IN LWR FWD PIT. CREW CLOSED BELL TESTED SYSTEM & FIRE INDICATION RETURNED. CREW DECLARED EMERGENCY & SHOT FIRE BOTTLE. A/C LANDED WITHOUT FURTHER INCIDENT. CFR CONFRIMED NO FIRE. PERFORMED LOWER CARGO COMPT SMOKE DETECTION SYSTEM ADJUSTMENT & T
- [SDR UPS02239943](https://openairdocs.org/sdr/UPS02239943.md): Pressure Panel · cracked · Nov 25, 2002 · N905UP · Boeing 72751C · Fuselage Main, Structure
  > INSPECTION TYPE:C SEVERAL CRACKS ON NLG WHEEL WELL PRESSURE WEB RHS FROM BS 260 DOWN 1 1" FROM CEILING AND 1" FWD OF THE AFT PRESSURE PANEL TP BS 279 6" BE LOW AFT PRESSURE PANEL DAMAGED AREAS REPAIRED IAW SRM51-40-2 FIG 1
- [SDR UPS02239946](https://openairdocs.org/sdr/UPS02239946.md): Pressure Panel · cracked · Nov 21, 2002 · N905UP · Boeing 72751C · Fuselage Main, Bulkhead
  > INSPECTION TYPE: C, NLG WHEEL WELL PRESSURE PANEL CRACKED AT BS 268, 3 INCHES DOWN FROM W/W CEILING. DAMAGED AREA CUTOUT IAW SRM 51-40-2 FIG 1 HFEC CONFIRMS A DEFECT FREE CONDITION, AREA REPAIR IAW SRM 51-40-2 F IG 1.
- [SDR UPS02239949](https://openairdocs.org/sdr/UPS02239949.md): Bolt · cracked · Nov 19, 2002 · N905UP · Boeing 72751C · Main Landing Gear Attach Section
  > INSPECTION TYPE: C, DURING REMOVAL OF LT HAND TRUNNION LINK, THE LT MAIN GEAR AFT TRUNNION BOLT AND TRUNNION HOUSING FOUND SHEARED. ON REMOVAL OF LT MLG, AFT BEARING MOUNTING JOURNAL FOUND CRACKED & PIECE BROKEN OFF. END OF JOURNAL.BEARING RETAINING BOLT SH
- [SDR UPS02239945](https://openairdocs.org/sdr/UPS02239945.md): Pressure Panel · cracked · Nov 19, 2002 · N905UP · Boeing 72751C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C SUSPECT CRACK ON NLG CEILING AT BS 273 LBL14. HFEC CONFIRMS CRACK, DAMAGED ARE CUTOUT IAW SRM 51-40-02 FIG, HFEC CONFIRMS NDF. REPAIR CARRIED OUT SRM 51-40-02 FIG 1.
- [SDR UPS02239944](https://openairdocs.org/sdr/UPS02239944.md): Pressure Panel · cracked · Nov 19, 2002 · N905UP · Boeing 72751C · Fuselage Main, Structure
  > INSPECTION TYPE:C CRACK ON NLG WHEEL WELL PRESSURE WEB @ BS 243.6 LHS 4" AFT FROM FWD PRESSURE PANEL. DAMAGED AREA CUT OUT IAW SRM 51-40-02 FIG1, HFEC AROUND CUTOUT NDF, REPAIR CARRIED OUT IAW SRM 51-40-02 FIG 1
- [SDR UPS02239940](https://openairdocs.org/sdr/UPS02239940.md): Fitting · cracked · Nov 18, 2002 · N905UP · Boeing 72751C · Fuselage Main, Structure
  > INSPECTION TYPE:C SUSPECT CRACK ON L/H BS 910 FITTING REPAIR CARRIED OUT IAW EO B727-5310-1896-B APPENDIX B
- [SDR UPS02239937](https://openairdocs.org/sdr/UPS02239937.md): Fitting · cracked · Nov 18, 2002 · N905UP · Boeing 72751C · Fuselage Main, Structure
  > INSPECTION TYPE:C SUSPECT CRACK ON RH BS 910 FITTING REPAIR CARRIED OUT IAW EO B727-5310-1896-B APPENDIX B
- [SDR UPS02239938](https://openairdocs.org/sdr/UPS02239938.md): Pin · corroded · Nov 16, 2002 · N905UP · Boeing 72751C · Horizontal Stabilizer Miscellaneous Structure
  > INSPECTION TYPE:C PITTING FOUND ON RT STAB INNER PINS. RT STAB INNER PIN REPLACED IAW MM 55-10-01.
- [SDR UPS02239950](https://openairdocs.org/sdr/UPS02239950.md): Spar · cracked · Nov 15, 2002 · N905UP · Boeing 72751C · Trailing Edge Flaps
  > INSPECTION TYPE: C, DURING LFEC INSPECTION OR RT INBOARD MID FLAP REAR SPAR UPPER CHORD, A CRACK WAS FOUND AROUND A FASTENER HOLE. REPAIRED PER EO.B727-5750-3582.
- [SDR UPS02239948](https://openairdocs.org/sdr/UPS02239948.md): Beam · cracked · Nov 15, 2002 · N905UP · Boeing 72751C · Fuselage Main, Structure
  > INSPECTION TYPE: C, DURING INSPECTION OF VERTICAL BEAM 17.8 RT, A CRACK WAS FOUND ON THE BEAM FLANGE. STOP CUT-OUT AT WL 273, BS 1183 REPAIR PARTS DRILLED OFF IAW EO B727-5310-11743. REPAIR ANGLES INSTALLED WET WITH SEALANT IAW EO B727-5310-11743 REPAIR
- [SDR UPS02239942](https://openairdocs.org/sdr/UPS02239942.md): Intercostal · cracked · Nov 15, 2002 · N905UP · Boeing 72751C · Fuselage Main, Structure
  > INSPECTION TYPE:C HORIZONTAL INTERCOSTAL CRACKED ON VERTICAL BEAM 17.8 L/H AT WL 283 1 183 BULKHEAD NEW INTERCOSTAL FABRICATED & INSTALLED PER BOEING DRAWING 65-16350 S HEET 6 & 65C15764 SH. 5 & SRM 51-30-2
- [SDR UPS02239941](https://openairdocs.org/sdr/UPS02239941.md): Floorbeam · cracked · Nov 14, 2002 · N905UP · Boeing 72751C · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C BEAM TIE CRACKED ON FLOORBEAM LWR FLANGE BS 328 RBL 40. REPAIR PLATE FABRICATED AND FITTED AS PER ARM 53-10-8.
- [SDR UPS02239947](https://openairdocs.org/sdr/UPS02239947.md): Fitting · cracked · Nov 13, 2002 · N905UP · Boeing 72751C · Fuselage Main, Attach Fittings
  > INSPECTION TYPE: C&SI, WHILE CARRY OUT HFEC INSPECTION ON LT BS 950 FITTING. CRACK FOUND IN ROW 1 UP PER FASTENER HOLE, COMMON TO STR 9. DISCREPANT HOLE REPAIRED IAW SMRO EO 2002-061-003 UPS ENG. FILE NO. B727-5310-17956
- [SDR UPS02239105](https://openairdocs.org/sdr/UPS02239105.md): Battery Pack · discharged · Aug 18, 2002 · N902UP · Boeing 72751C · Emergency Lighting
  > INSPECTION TYPE:N/A BOTH EMERGENCY LIGHT BATTERY PACKS LOW. REMOVED AND REPLACED BATTERY, OPS CHECK NORMAL.
- [SDR CA020809002](https://openairdocs.org/sdr/CA020809002.md): Limiter · cracked · Aug 8, 2002 · Boeing 72751C · Hydraulic System, Main
  > (CAN) SYSTEM "A" HYDRAULIC FAILURE ON SHORT FINAL. MAINTENANCE FOUND OUTBOARD FLAP FLOW LIMITING VALVE CRACKED. REPLACED.
- [SDR UPS02238710](https://openairdocs.org/sdr/UPS02238710.md): Relay · failed · Jun 28, 2002 · N905UP · Boeing 72751C · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY LIGHTS ABOVE COCKPIT DOOR ILLUMINATED IN FLIGHT WITH ARM SWITCH IN THE ARMED POSITION. REMOVED R70 RELAY. OPS CHECKS GOOD.
- [SDR UPS02238629](https://openairdocs.org/sdr/UPS02238629.md): Battery · discharged · Jun 13, 2002 · N903UP · Boeing 72751C · Emergency Lighting
  > INSPECTION TYPE:PFLT CABIN DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERIES BOTH EMERGENCY LIGHTS, OPS CHECK NORMAL.
- [SDR UPS02238096](https://openairdocs.org/sdr/UPS02238096.md): Rack · loose · Apr 26, 2002 · N903UP · Boeing 72751C · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS ILLUMINATED SEVERAL TIMES DURING FLIGHT. FLIGHT DECK EMERGENCY LIGHT MOUNTING RACK TIGHTENED, EMERGENCY LIGHTING CHECK SERV PER MM 33-50-67.
- [SDR UPS02237566](https://openairdocs.org/sdr/UPS02237566.md): Light · defective · Feb 4, 2002 · N903UP · Boeing 72751C · Emergency Lighting
  > INSPECTION TYPE:N/A L1 DOOR EMERGENCY EXIT LIGHT COMES ON DIM AND GOES OUT IN LESS THAN A MINUTE. REMOVED AND REPLACED L1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY SYSTEM, GROUND CHECKS GOOD.
- [SDR UPS01237043](https://openairdocs.org/sdr/UPS01237043.md): Bullet · cracked · Oct 14, 2001 · N902UP · Boeing 72751C · Turbine Engine Air Inlet Section
  > INSPECTION TYPE:S-10 ENGINE 3 SPINNER CRACK FOUND DURING SEG-10 CHECK. HAS 1 INCH CRACK AT BOLT HOLE. REMOVED AND REPLACED NR 3 ENG SPINNER FAIRING IAW MM 72-30-10. OPS NORMAL AT THIS TIME.
- [SDR UPS01237045](https://openairdocs.org/sdr/UPS01237045.md): Clip · defective · Oct 13, 2001 · N903UP · Boeing 72751C · Emergency Equipment
  > INSPECTION TYPE: MAIN ENTRY SLIDE INOP. REPLACED BOTH BAR RETAINER CLIPS, P/N 65-64828-3, REINSTALLED SLIDE.
- [SDR UPS01237044](https://openairdocs.org/sdr/UPS01237044.md): Smoke Detector · faulty · Oct 12, 2001 · N902UP · Boeing 72751C · Smoke Detection
  > INSPECTION TYPE: LOWER CARGO SMOKE DETECTOR SYS MX LIGHT ILLUMINATED. REMOVED AND REPLACED TWO SMOKE DETECTORS REF MM 26/18/00 S/N IN FWD 11363 S/N OUT FWD 3740 S/N IN AFT 2356 S/N OUT AFT 5107.
- [SDR UPS01236823](https://openairdocs.org/sdr/UPS01236823.md): Light · inoperative · Sep 15, 2001 · N902UP · Boeing 72751C · Emergency Lighting
  > INSPECTION TYPE:IN CABIN ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT IAW B727 MM 33-50-101 OPS CHECKS GOOD.
- [SDR UPS01236733](https://openairdocs.org/sdr/UPS01236733.md): Stiffener · cracked · Aug 30, 2001 · N905UP · Boeing 72751C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:N/A RT MLG ACT BEAM SUPPORT PANEL. FWD STIFFENER CRACKED AT INBD HINGE. REPAIRED CRACKED STIFFENER RT MLG ACT BEAM SUPPORT PANEL PER B727 SRM 51-40-3
- [SDR UPS01236532](https://openairdocs.org/sdr/UPS01236532.md): Slide · inoperative · Aug 5, 2001 · N905UP · Boeing 72751C · Escape Slide
  > INSPECTION TYPE:IN MAIN CABIN SLIDE INOP REF DEF M220206 FWD ENTRY SLIDE DEPLOYED. REPLACED SLIDE AND LATCH ASSY REF 25-60-14.
- [SDR 2001F00219](https://openairdocs.org/sdr/2001F00219.md): Valve · inoperative · Jul 22, 2001 · N413EX · Boeing 72751C · Fuel Controlling System
  > ON APPROACH, AFTER THROTTLES WERE RETARDED, NR 1 ENGINE SPOOLED DOWN AS NORMAL. WHEN POWER WAS APPLIED, NR 1 ENGINE FAILED TO SPOOL UP. AFTER LANDING, NR 1 THROTTLE WAS CYCLED BACK AND FORTH WITH N1, N2 OR FUEL FLOW. ENGINE HAD SHUT DOWN. NR 1 GENERATOR TH
- [SDR UPS01236244](https://openairdocs.org/sdr/UPS01236244.md): Light · discharged · Jul 5, 2001 · N904UP · Boeing 72751C · Emergency Lighting
  > INSPECTION TYPE:PFLT COCKPIT EMERGENCY LIGHT ABOVE DOOR VERY DIM. REMOVED AND REPLACED BATTERIES, OPS CHECK OK AS PER MM 33-50-01.
- [SDR UPS01236026](https://openairdocs.org/sdr/UPS01236026.md): Panel · cracked · May 31, 2001 · N905UP · Boeing 72751C · Wing, Plate/Skin
  > INSPECTION TYPE:C, 1 INCH CRACK ON PANEL, UPPER SURFACE OF WING, JUST FWD OF I/B AILERON ON RIGHT WING, I/B EDGE OF PANEL. REPAIRED PER SRM 51-40-2.
- [SDR UPS01236033](https://openairdocs.org/sdr/UPS01236033.md): Skin · cracked · May 30, 2001 · N905UP · Boeing 72751C · Spoilers
  > INSPECTION TYPE:C, CRACK FOUND IN TRAILING EDGE SKIN ADJACENT NR 3 SPOILER PANEL HINGE INBOARD HINGE. CRACK REPAIRED IAW SRM.
- [SDR UPS01235942](https://openairdocs.org/sdr/UPS01235942.md): Light · inoperative · May 21, 2001 · N905UP · Boeing 72751C · Emergency Lighting
  > INSPECTION TYPE:IN EMERGENCY LIGHTS UNARMED LIGHT INOP WHEN UNARMED AND PRESS TO TEST. RELAMPED AND FUNCTIONALLY CK GOOD AS PER 33-50.
- [SDR UPS01235785](https://openairdocs.org/sdr/UPS01235785.md): Warning System · inoperative · May 2, 2001 · N904UP · Boeing 72751C · Detection System
  > COMPT SHOWS-TD DELAY FOR FIRE WARNING BELL INDICATOR INOP COCKPIT FIRE BELL WILL NOT SOUND WITH THE ENG FIRE DETECTION PANEL TEST SWITCH IN A,B,OR A/B THIS APPLIES TO ACTUATING EITHER THE ENG TEST SWITCH OR WHEEL WELL TEST SWITCH. CLEANED AND RESECURED WIR
- [SDR 20010524SG001](https://openairdocs.org/sdr/20010524SG001.md): Light · inoperative · Apr 28, 2001 · N417EX · Boeing 72751C · Smoke Detection
  > FOUND UPPER LEFT LIGHT BULB IN MAIN CABIN SMOKE DETECTOR IS BURNED OUT. REMOVED AND REPLACED LEFT AND RIGHT BULBS IN MAIN CABIN SMOKE DETECTOR. (M)
- [SDR UPS01235508](https://openairdocs.org/sdr/UPS01235508.md): Battery · discharged · Apr 4, 2001 · N902UP · Boeing 72751C · Emergency Lighting
  > BOTH EMERGENCY EXIT LIGHT BATTERY PACK LIGHTS VERY DIM FADE TO NEAR FAILURE IN 30 SECONDS. REPLACED BOTH BATTERIES IN BOTH LIGHT PACKS AS REQUIRED STEADY ILLUMINATION OPS CK OK
- [SDR UPS01235220](https://openairdocs.org/sdr/UPS01235220.md): Strap · unserviceable · Mar 6, 2001 · N904UP · Boeing 72751C · Passenger/Crew Doors
  > INSPECTION TYPE:IN FWD ENTRY DOOR HANDLE STRAP IS NOT LONG ENOUGH TO ENGAGE VELCRO PAD WHEN LOOPED AROUND THE DOOR HANDLE. REMOVED FWD ENTRY DOOR HANDLE STRAP AS PER EO B727-2560-12064. OK FOR SERVICE.
- [SDR UPS01235105](https://openairdocs.org/sdr/UPS01235105.md): Switch · out of adj · Feb 26, 2001 · N904UP · Boeing 72751C · Landing Gear Position and Warning
  > INSPECTION TYPE:N/A ATB-AIR/GROUND SAFETY SENSOR FAILED IN GROUND ILLEG BUT LANDING GEAR RETRACTED NORMALLY. REPOSITION MAIN GEAR SAFETY SWITCH ILLEG AND PERFORMED SWITCH OPS CHECK AS PER B727 M/M 32-0211. NO DEFECTS NOTED.
- [SDR 20010425AP002](https://openairdocs.org/sdr/20010425AP002.md): Battery · discharged · Feb 22, 2001 · N413EX · Boeing 72751C · Smoke Detection
  > FOUND LOWER CARGO SMOKE DETECTOR PANEL, AMBER MAINTENANCE LIGHT ILLUMINATED. REMOVED AND REPLACED BATTERIES IN FORWARD AND AFT CARGO COMPARTMENTS SMOKE DETECTORS. SYSTEM TEST NORMAL. (M)
- [SDR UPS01235205](https://openairdocs.org/sdr/UPS01235205.md): Panel · cracked · Feb 19, 2001 · N904UP · Boeing 72751C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, NOSE WHEEL WELL LT SIDEWALL LOWER CHORD COVER PANEL SHOWS CRACK INDICATION 2 AROUND RIVET HEADS. REMOVED PANEL AND MADE NEW PER SAMPLE AND INSTALLED AS PER B727 SRM 51-30-2.
- [SDR UPS01235203](https://openairdocs.org/sdr/UPS01235203.md): Pressure Panel · cracked · Feb 19, 2001 · N904UP · Boeing 72751C · Fuselage Main, Structure
  > INSPECTION TYPE:C, NOSE WHEEL WELL BS 227.8 FWD WALL BL 0 CRACK INDICATION AROUND ROW OF FASTENER HEADS. CUT OUT DAMAGE AREA AS PER B727 SRM 51-40-2 & 51-10-1, INSTALLED DOUBLER REPAIR AS PER B727 51-40-2.
- [SDR UPS01235202](https://openairdocs.org/sdr/UPS01235202.md): Pressure Panel · cracked · Feb 19, 2001 · N904UP · Boeing 72751C · Fuselage Main, Structure
  > INSPECTION TYPE:C, NOSE WHEEL WELL RT SIDEWALL BS 248 LWR OF FWD ACCESS DOOR CRACK INDICATION AROUND FASTENER HEAD. CUT OUT DAMAGE AREA AS PER B727 SRM 51-40-2 & 51-10-1. INSTALLED DOUBLER REPAIR AS PER B727 SRM 51-40-2.
- [SDR UPS01235201](https://openairdocs.org/sdr/UPS01235201.md): Pressure Panel · cracked · Feb 19, 2001 · N904UP · Boeing 72751C · Fuselage Main, Structure
  > INSPECTION TYPE:C, NOSE WHEEL WELL RT SIDEWALL BS 264.3 WL 154 LWR OF AFT ACCESS DOOR CRACK INDICATION ALONG ROW OF RIVET HEADS. CUT OUT DAMAGE AREA AS PER B727 SRM 51-40-2 & 51-10-1. INSTALLED DOUBLER REPAIR AS PER B727 SRM 51-40-2 MAT USED 2024-T3.050 30,
- [SDR UPS01235199](https://openairdocs.org/sdr/UPS01235199.md): Pressure Panel · cracked · Feb 19, 2001 · N904UP · Boeing 72751C · Fuselage Main, Structure
  > INSPECTION TYPE:C, NOSE WHEEL WELL RT SIDE WALL BS 259.5 FWD OF AFT ACCESS DOOR CRACK INDICATION ALONG ROW OF RIVET HEADS. CUT OUT DAMAGE AREA AS PER B727 SRM 51-40-2, INSTALLED DOUBLER. REPAIR PER SRM 51-40-20.
- [SDR UPS01235200](https://openairdocs.org/sdr/UPS01235200.md): Angle · corroded · Feb 14, 2001 · N904UP · Boeing 72751C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C-CK, AFT AIRSTAIR SUPPORT ANGLE CORROSION UNDER 4TH STEP FROM TOP. REMOVED AND REPLACED CHORD SUPPORT ANGLE ON AFT AIRSTAIRS.
- [SDR UPS01235208](https://openairdocs.org/sdr/UPS01235208.md): Bracket · cracked · Feb 13, 2001 · N904UP · Boeing 72751C · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C-CK, TAIL SKID COMPT, 2 UPPER SUPPORT RODS AFT ATTACH BRACKETS, LT AND RT CRACKED. REMOVED AND REPLACED BOTH LT AND RT ATTACH BRACKETS FOR TAIL SKID UPPER SUPPORT RODS.
- [SDR 20010315SG001](https://openairdocs.org/sdr/20010315SG001.md): Motor · failed · Feb 13, 2001 · N436EX · Boeing 72751C · Trailing Edge Flap Actuator
  > FLT 733 - EN ROUTE TO ORD HAD A SPLIT FLAP INDICATION. AIR CREW CONDUCTED AN AIR TURN BACK TO SEA. AIR CREW DUMPED FUEL AND DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFELY AND WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED OUTBOARD FLAP ALTERNATE DRIVE ELECT

Next page: https://openairdocs.org/model/boeing-727-51c/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 = '72751C'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-51c/reports

---
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