# Service difficulty reports: Boeing 747-281F

A list on [Boeing 747-281F](https://openairdocs.org/model/boeing-747-281f.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 52 reports

- [SDR Q2SA20120930197](https://openairdocs.org/sdr/Q2SA20120930197.md): Battery Pack · discharged · Sep 30, 2012 · N783SA · Boeing 747281F · Emergency Lighting
  > EMERGENCY FLOOR LIGHTING IN UPPER DECK INOP. REMOVED AND REPLACED BATTERY PACK CARTRIDGE IAW 3-51-04. SYS OPS CHECK NORMAL.
- [SDR Q2SA201209301](https://openairdocs.org/sdr/Q2SA201209301.md): Battery Pack · defective · Sep 30, 2012 · N783SA · Boeing 747281F · Emergency Lighting
  > EMERGENCY LIGHT IN THE COCKPIT INTERMITTENT. REMOVED AND REPLACED BATTERY PACK AND CHARGER ASSY IAW 33-51-07. SYSTEM OPS CHECK NORMAL.
- [SDR Q2SA2012091178305](https://openairdocs.org/sdr/Q2SA2012091178305.md): Generator · failed · Sep 11, 2012 · N783SA · Boeing 747281F · AC Generator-Alternator
  > WHILE EN ROUTE FROM MIA TO ANC EXPERIENCED A NR 1 AND NR 3 GENERATOR FAILURE. THEREAFTER DISPATCH WAS NOTIFIED BY THE CREW, THE AIRCRAFT HAD LOST A THIRD GENERATOR. SHORTLY AFTER THAT THEY LOST THE FOURTH AND FINAL AIRCRAFT GENERATOR JUST BEFORE LANDING. TH
- [SDR Q2SA2012072875813](https://openairdocs.org/sdr/Q2SA2012072875813.md): Skin · failed · Jul 28, 2012 · N758SA · Boeing 747281F · Fuselage Main, Plate/Skin
  > DURING POST-FLIGHT, FOUND A HOLE AND CRACK DAMGE AT SECTION 48 LH SIDE BETWEEN STATION 2638 AND 2658 AND S-11L AND S-13L. STRINGER (P/N 65B 02976-1) CHORD (P/N 65B02515-113) AND ANGLE (P/N 65B02712-139) ASSEMBLIES WERE FOUND TO BE DAMAGED BEYOND ALLOWABLE LIMI
- [SDR TX9Y20111214011](https://openairdocs.org/sdr/TX9Y20111214011.md): Cargo Track · cracked · Dec 11, 2011 · N758SA · Boeing 747281F · Fuselage, Seat/Cargo Attach Fittings
  > FORWARD CARGO TRACK FORWARD RIGHT CORNER WAS FOUND CRACKED. REPAIRED AS PER SRM 53-10-05 FIG 5 REV 120.
- [SDR TX9Y20111208008](https://openairdocs.org/sdr/TX9Y20111208008.md): Structure · corroded · Dec 7, 2011 · N758SA · Boeing 747281F · Trailing Edge Flaps
  > LT WING T/E INBOARD MID FLAP T/E LOWER CHORD WAS FOUND CORROSION. THREE CORROSION AREAS WERE FOUND ON LEFT T/E INBOARD MID FLAP (P/N:65B02025-35) T/E LOWER CHORD (P/N:65B02098-1) HORIZONTAL FLANGE LOWER SURFACE. THE REPAIR WAS CARRIED OUT PER BOEING MESSAGE
- [SDR TX9Y20111208009](https://openairdocs.org/sdr/TX9Y20111208009.md): Mount · corroded · Dec 7, 2011 · N758SA · Boeing 747281F · Engine Mount Section
  > NR 4 ENG AFTER UPPER ENG MOUNT UPPER SURFACE WAS FOUND RUSTED HEAVILY. NR 4 ENGINE AFTER ENGINE MOUNT WAS REPLACED AS PER AMM 71-21-03 REV 86.
- [SDR TX9Y20111208010](https://openairdocs.org/sdr/TX9Y20111208010.md): Skin · cracked · Dec 7, 2011 · N758SA · Boeing 747281F · Fuselage Main, Plate/Skin
  > DURING REMOVING TWO ADDITIONAL DOUBLERS, THREE HOLE CRACK ON THE LEFT DOUBLER FUSELAGE SKIN AND TWO HOLE CRACK ON THE RIGHT DOUBLER FUSELAGE SKIN WERE FOUND. FOR EXISTING REPAIR DOUBLERS WHICH COMMON TO NOSE WHEEL WELL AFTER CORNER SKIN BETWEEN STA 400 TO STA
- [SDR TX9Y20111207007](https://openairdocs.org/sdr/TX9Y20111207007.md): Longeron · cracked · Dec 5, 2011 · N758SA · Boeing 747281F · Engine Cowling System
  > DURING INSPECTION OF NR 3 ENGINE RT SIDE COWL, ONE CRACK AND ONE DEEP CHAFING DAMAGE WERE FOUND AT LOWER LONGERON (P/N:65B94280-199). THE REPAIR WAS PERFORMED AS PER BOEING MESSAGE NUMBER TEC-SOF-11-0102.
- [SDR TX9Y20111206004](https://openairdocs.org/sdr/TX9Y20111206004.md): Skin · dented · Dec 4, 2011 · N758SA · Boeing 747281F · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN (STA2200-STA2400,STR27-STR28) WAS FOUND ONE ORIGINAL REPAIR RIVET AND DENT. FUSELAGE SKIN DOUBLER WAS REPAIRED AS PER SRM 53-30-03 FIG 4 REV 120.
- [SDR TX9Y20111205003](https://openairdocs.org/sdr/TX9Y20111205003.md): Failsafe · corroded · Dec 3, 2011 · N758SA · Boeing 747281F · Fuselage Main, Frame
  > DURING DATUM AIRCRAFT INPUT,A CORROSION (SIZE ABOUT:3.3"*0.8") WAS FOUND ON BULK CARGO FRAME LOWER LOBE FAIL SAFE CHORD (P/N:65B04347-149,STA2200) HORIZONTAL FLANGE AT STR 40R. THE REPAIR WAS PERFORMED PER BOEING MESSAGE NUMBER TEC-SOF-11-0099. THE REPAIR WA
- [SDR TX9Y20111202001](https://openairdocs.org/sdr/TX9Y20111202001.md): Skin · dented · Dec 1, 2011 · N758SA · Boeing 747281F · Cargo/Baggage Doors
  > BULK CARGO DOOR SKIN FORWARD LOWER CORNER WAS FOUND A DENT. THE SKIN SMOOTHED OUT WAS FOUND OUT LIMITS. BULK CARGO DOOR SKIN DENT AREA WAS REPAIRED AS PER SRM 52-00-03 FIG 9 REV 120.
- [SDR TX9Y20111202002](https://openairdocs.org/sdr/TX9Y20111202002.md): Doubler · cracked · Dec 1, 2011 · N758SA · Boeing 747281F · Spoilers
  > NR 9 SPOILER HINGE DOUBLER AND NR 11 SPOILER HINGE DOUBLER WERE FOUND CRACKED. NR 9 SPOILER AND NR 11 SPOILER WERE REPLACED AS PER AMM 27-61-02 REV 86.
- [SDR TX9Y20111121010](https://openairdocs.org/sdr/TX9Y20111121010.md): Access Panel · damaged · Nov 18, 2011 · N783SA · Boeing 747281F · Fuselage Miscellaneous Structure
  > MAIN DECK MEC BAY ACCESS PANEL ASSY (P/N:65B11970-35) LOWER SURFACE WAS FOUND DENTS AND PUNCTURE HOLE, AND AT THE ACCESS PANEL (P/N:65B16167-14) CORNERS WAS FOUND CHIPPED OFF. THE REPAIR WAS PERFORMED PER BOEING MESSAGE NUMBER TEC-SOF-11-0097 AND SRM 51-40-20
- [SDR TX9Y20111116009](https://openairdocs.org/sdr/TX9Y20111116009.md): Tension Tie · cracked · Nov 14, 2011 · N783SA · Boeing 747281F · Fuselage Miscellaneous Structure
  > UPPER DECK TENSION TIE STA 860 RT FAIL SAFE CHORD WAS FOUND CRACK. UPPER DECK TENSION TIE STA 860 RT FAIL SAFE CHORD WAS REPAIRED PER SRM 51-40-03 FIG 2 REV 120. THE REPAIR IS APPROVED FOR 24 MONTHS.
- [SDR TX9Y20111115008](https://openairdocs.org/sdr/TX9Y20111115008.md): Tension Tie · cracked · Nov 14, 2011 · N783SA · Boeing 747281F · Fuselage Miscellaneous Structure
  > UPPER DECK STA 800 LT & RT FWD CHANNEL OF TENSION TIE WAS FOUND CRACK. UPPER DECK STA 840 LT FWD CHANNEL OF TENSION TIE WAS FOUND CRACK. UPPER DECK STA 860 RT TENSION TIE WAS FOUND CRACK. UPPER DECK TENSION TIES (STA 800 LT & RT, STA 840 LT AND STA 860 RT)
- [SDR TX9Y20111114007](https://openairdocs.org/sdr/TX9Y20111114007.md): Structure · damaged · Nov 11, 2011 · N783SA · Boeing 747281F · Wing Miscellaneous Structure
  > ONE ELONGATED HOLE WAS FOUND COMMON TO RT INBOARD FIXED TRAILING EDGE BEAM UPPER CHORD (P/N:65B11614) AT APPROX WBL 235.20. THE REPAIR WAS CARRIED OUT PER BOEING MESSAGE NUMBER TEC-SOF-11-0077 AND SRM 51-10-02. DETAILS OF THE REPAIR ARE RECORDED IN EN EA-57-
- [SDR TX9Y20111111006](https://openairdocs.org/sdr/TX9Y20111111006.md): Doubler · corroded · Nov 8, 2011 · N783SA · Boeing 747281F · Fuselage Main, Plate/Skin
  > WATER SERVICE PORT EXTERIOR DOUBLER WAS FOUND CORROSION (BS 980-BS 1000, STR 44R-STR 46R). THE CORROSION WAS REMOVED AS PER SRM 51-10-01 REV 120. THE CORROSION WAS BLENDED OUT, NOT WITHIN SRM 53-30-01 REV 120 LIMITS. THE NEW WATER SERVICE PORT EXTERIOR DOUBLE
- [SDR TX9Y20111111005](https://openairdocs.org/sdr/TX9Y20111111005.md): Shear Tie · cracked · Nov 8, 2011 · N783SA · Boeing 747281F · Wing Spar
  > WING CENTER SECTION FRONT SPAR LOCATION RBBL 33.89 SHEAR TIE (P/N:69B14267-9) WAS FOUND CRACK. A NEW SHEAR TIE WAS FABRICATED AS PER DRAWING 69B14267-9. THE REWORK OF TWO TAPER HOLES WAS PERFORMED PER BOEING MESSAGE NUMBER TEC-SOF-11-0096 AND SRM 51-30-05. DE
- [SDR TX9Y20111111004](https://openairdocs.org/sdr/TX9Y20111111004.md): Panel · damaged · Nov 8, 2011 · N783SA · Boeing 747281F · Nacelle/Pylon Miscellaneous Structure
  > ONE ELONGATED HOLE WAS FOUND COMMON TO DOOR PANEL (P/N:65B90719-86) OF NR 1 PYLON INBOARD TRAILING EDGE FAIRING DOOR ASSY (P/N:65B90717) AT APPROX STA 297.5. THE REPAIR WAS PERFORMED PER BOEING MESSAGE NUMBER TEC-SOF-11-0078 AND SRM 51-10-01. DETAILS OF THE
- [SDR TX9Y20111108003](https://openairdocs.org/sdr/TX9Y20111108003.md): Flap Track · corroded · Nov 5, 2011 · N783SA · Boeing 747281F · Trailing Edge Flaps
  > FLAP TRACK NR 4 FORWARD END CLEVIS INBOARD LUG SURFACE FOUND CORROSION INDICATION ON INBOARD LUG INBOARD SURFACE. THE REPAIR WAS PERFORMED PER BOEING MESSAGE NUMBER TEC-SOF-11-0092 AND SB 747-57-2307 REVISION 2. THE DEVIATION WAS APPROVED UNDER ODA-300064-NM
- [SDR TX9Y20111104002](https://openairdocs.org/sdr/TX9Y20111104002.md): Structure · cracked · Nov 1, 2011 · N783SA · Boeing 747281F · Nacelle/Pylon, Main Frame
  > CRACK INDICATIONS FOUND ON NR 2 PYLON STRUT STRUCTURE. REPAIRED PER MN TEC-SOF-11-0088, SRM 51-10-01 AND SRM 51-40-02.
- [SDR TX9Y20111104001](https://openairdocs.org/sdr/TX9Y20111104001.md): Splice Plate · cracked · Nov 1, 2011 · N783SA · Boeing 747281F · Horizontal Stabilizer Structure
  > A FASTENER HOLE WAS FOUND CRACKED AT HORIZONTAL STABILIZER CENTER SECTION LT SIDE LOWER SPLICE PLATE. REPLACED PER MN TEC-SOF-11-0082 AND SRM 51-30-05.
- [SDR Q2SA783004](https://openairdocs.org/sdr/Q2SA783004.md): Duct · cracked · Sep 2, 2011 · N783SA · Boeing 747281F · Pneumatic Distribution System
  > NR 3 ENG FIRE WARNING LIGHT ILLUM WHILE ADVANCING POWER TO 88% RPM. BOTH NR 3 ENG NACELLE IND WERE AT 10 UNITS. EGT WAS RISING THRU 800 DEG CELCIUS WHILE OTHER ENG WERE AT APPROX 700 DEG CELSIUS. AIRSPEED WAS 200 KTS, 3500 FT MSL, LEVEL, FLAPS 5 CONFIG. EN
- [SDR Q2SA758012](https://openairdocs.org/sdr/Q2SA758012.md): Engine · failed · Sep 24, 2010 · N758SA · Boeing 747281F · Engine (Turbine/Turboprop)
  > FLIGHT MAS6145, WHILE PREPARING FOR TAKEOFF, EXPERIENCED AN UNCONTAINED ENGINE FAILURE.
- [SDR Q2SA795002A](https://openairdocs.org/sdr/Q2SA795002A.md): Actuator · missing · Aug 24, 2010 · N758SA · Boeing 747281F · Landing Gear Actuator
  > ACFT 795 DEPARTED AS FLT SOO113, BOTH TAXI & TAKEOFF OPS WERE NORMAL. MLG HANDLE SELECTED TO "UP" POSITION AFTER LIFTOFF. BOTH RED "DOOR OPEN" & "RED "GEAR" LIGHTS REMAINED ILLUMINATED. FO CONTINUED FLYING & CLIMBED ON COURSE. CAPTAIN & FE COMPLETED QRH PROCED
- [SDR Q2SA758011](https://openairdocs.org/sdr/Q2SA758011.md): Engine · leaking · Jul 22, 2010 · N758SA · Boeing 747281F · Turbine Engine Oil System
  > DURING THE TAKEOFF ROLL IN OMDB NR 1 EGT GAUGE BRIEFLY WENT TO 0, THEN RETURNED TO NORMAL. DURING THE CLIMB TO FL 300 IT WAS NOTICED, NR 1 EGT WAS RUNNING SIGNIFICANTLY HOTTER (APPROXIMATELY 80 DEG C) THAN THE OTHERS. AT THE TOP OF CLIMB, THE NR 1 EGT KEPT C
- [SDR VGQY2010051800005](https://openairdocs.org/sdr/VGQY2010051800005.md): Mount · corroded · May 18, 2010 · N820SA · Boeing 747281F · Engine Mount Section
  > DRWS NR 0020, NR 3 ENGINE AFT. UPPER MOUNT FOUND RUST. REMOVED AND REPROTECTED PER OHM CMM 71-20-02. MATERIAL REMOVED = 0.008", FOUND WITHIN LIMITS PER OHM CMM 71-20-02.
- [SDR 2010FA0000346](https://openairdocs.org/sdr/2010FA0000346.md): Hinge Fitting · cracked · Apr 15, 2010 · N758SA · Boeing 747281F · Horizontal Stabilizer, Attach Fittings
  > HORIZ STABILIZER LT 2 PLACES 0.9 INCH AND 0.8 INCH & RT 2 PLACES 1.1 INCH AND 0.85 INCH, HINGE FITTING CRACKED.
- [SDR 2010FA0000345](https://openairdocs.org/sdr/2010FA0000345.md): Stiffener · cracked · Apr 15, 2010 · N758SA · Boeing 747281F · Nacelle/Pylon Miscellaneous Structure
  > PYLON NR 2 INBD NR 3 STIFFENER CRACK 0.67 INCH BETWEEN NAC STA 248 AND NAC STA 259 ON THE RT SIDE.
- [SDR 2010FA0000344](https://openairdocs.org/sdr/2010FA0000344.md): Skin · corroded · Apr 15, 2010 · N758SA · Boeing 747281F · Fuselage Main, Plate/Skin
  > FWD CARGO LOWER FUSELAGE SKIN AT STA 1000 WAS CORRODED LEVEL 2.
- [SDR 2010FA0000343](https://openairdocs.org/sdr/2010FA0000343.md): Doubler · cracked · Apr 15, 2010 · N758SA · Boeing 747281F · Passenger/Crew Doors
  > MAIN ENTRY DOOR NR 1 UPPER OUTER SKIN DOUBLER CRACK, 0.35 INCH AT UPPER HINGE DOOR.
- [SDR 2010FA0000342](https://openairdocs.org/sdr/2010FA0000342.md): Stiffener · cracked · Apr 15, 2010 · N758SA · Boeing 747281F · Nacelle/Pylon, Main Frame
  > PYLON NR 1, INBD NR 3, STIFFENER CRACK.
- [SDR VGQY2010041300005](https://openairdocs.org/sdr/VGQY2010041300005.md): Skin · damaged · Apr 13, 2010 · N783SA · Boeing 747281F · Fuselage Main, Plate/Skin
  > COMPLIED WITH EN 1040-10, PERMANENT REPAIR FOR SKIN DAMAGE AT STA 520 T0 STA 700 BETWEEN S-39R TO S-42R.
- [SDR VGQY2010041400006](https://openairdocs.org/sdr/VGQY2010041400006.md): Skin · damaged · Apr 13, 2010 · N783SA · Boeing 747281F · Fuselage Main, Plate/Skin
  > REQUEST PERMANENT REPAIR ON BELLY SKIN AT STA 520 - 540 STR 38R - 42R IAW SRM 783-007. COMPLIED WITH EN 1040-10, PERMANENT REPAIR FOR SKIN DAMAGE AT STA 520 T0 STA 700 BETWEEN S-39R TO S-42R.
- [SDR VGQY2010041400005](https://openairdocs.org/sdr/VGQY2010041400005.md): Skin · damaged · Apr 13, 2010 · N783SA · Boeing 747281F · Fuselage Main, Plate/Skin
  > REQUEST PERMANENT REPAIR ON BELLY SKIN AT STA 670-700 S37-42R IAW REP 783-024 PAGE 1 OF 4. REF: RAP 783-007. COMPLIED WITH EN 1040-10, PERMANENT REPAIR FOR SKIN DAMAGE AT STA 520 T0 STA 700 BETWEEN S-39R TO S-42R.
- [SDR VGQY2010041400004](https://openairdocs.org/sdr/VGQY2010041400004.md): Mount · corroded · Apr 13, 2010 · N783SA · Boeing 747281F · Engine Mount Section
  > NR 4 ENG PYLON, LOWER AFT MOUNT FOUND WITH SURFACE CORROSION. REMOVED AND REPLACED NR 4 ENGINE AFT LOWER ENGINE MOUNT AS PER AMM 71-21-04 REV 84.
- [SDR VGQY2010041400003](https://openairdocs.org/sdr/VGQY2010041400003.md): Mount · corroded · Apr 13, 2010 · N783SA · Boeing 747281F · Engine Mount Section
  > NR 4 ENG PYLON, UPPER AFT MOUNT FOUND WITH SURFACE CORROSION. REMOVED AND REPLACED NR 4 ENGINE AFT UPPER ENGINE MOUNT AS PER AMM 71-21-04 REV 84.
- [SDR VGQY2010041300002](https://openairdocs.org/sdr/VGQY2010041300002.md): Structure · corroded · Apr 13, 2010 · N783SA · Boeing 747281F · Fuselage Main, Structure
  > STA 1920 FRAME BULB TEE 65B04333-89 VERTICAL FLANGE IS FOUND CRACKED AND CHIPPED OFF AT RBL 6.30. COMPLIED WITH EN 1044-10, REPAIR FOR CRACKED 65B0433-89 BULB TEE VERTICAL FLANGE AT STA 1920 FRAME RBL 6.30.
- [SDR Q2SA758010](https://openairdocs.org/sdr/Q2SA758010.md): Doubler · cracked · Apr 12, 2010 · N758SA · Boeing 747281F · Passenger/Crew Doors
  > MAIN ENTRY DOOR NR 1 UPPER OUTER SKIN DOUBLER CRACK AT UPPER HINGE DOOR.
- [SDR Q2SA758009](https://openairdocs.org/sdr/Q2SA758009.md): Stiffener · cracked · Apr 12, 2010 · N758SA · Boeing 747281F · Nacelle/Pylon Miscellaneous Structure
  > PYLON NR 1 INBOARD NR 3 STIFFENER CRACK.
- [SDR VGQY2010041300001](https://openairdocs.org/sdr/VGQY2010041300001.md): Stiffener · corroded · Apr 12, 2010 · N783SA · Boeing 747281F · Horizontal Stabilizer Miscellaneous Structure
  > RIGHT HORIZONTAL STABILIZER REAR SPAR AT ELEVATOR STATION 206.8 STIFFENER LOWER END FOUND CORRODED. COMPLIED WITH EN 1048-10, ALTERNATIVE FABRICATION FOR HORIZONTAL STAB REAR SPAR ATTACHED ANGLE 65B03779-12.
- [SDR Q2SA758008](https://openairdocs.org/sdr/Q2SA758008.md): A/C Pack · vibration · Nov 13, 2009 · N758SA · Boeing 747281F · Cabin Cooling System
  > DEPARTURE FROM VAKK TO VMCC: AFTER TAKEOFF NR 1 AIR CONDITIONING PACK STARTED SEVERE RUMBLING NOISE AND EMITTED AN ODOR. AIRCRAFT QUICK HANDBOOK PROCEDURE ACCOMPLISHED. REMOVED AND REPLACED ACM AND DUCT ASSEMBLY. OPERATIONAL AND LEAK CHECK ACCOMPLISHED AND
- [SDR Q2SA783003](https://openairdocs.org/sdr/Q2SA783003.md): Hydraulic Line · ruptured · Oct 31, 2009 · N783SA · Boeing 747281F · Hydraulic System, Main
  > AFTER TAKING OFF FROM KDOV, NR 1 HYDRAULIC SYSTEM QUANTITY DECREASED RAPIDLY, CREW RAN ABNORMAL CHECKLIST IN ACCORDANCE WITH B-747-200/300 QUICK REFERENCE HANDBOOK. CONTINUED FLIGHT AND LANDED SAFELY AT KJFK. AFTER LANDING MAINTENANCE CREW FOUND A RUPTURED H
- [SDR Q2SA758007](https://openairdocs.org/sdr/Q2SA758007.md): Fuel Filter · failed · Oct 24, 2009 · N758SA · Boeing 747281F · Engine Fuel Distribution
  > ON TAKEOFF CLIMBOUT OF KJFK, ENGINE NR 1 AND ENGINE NR 4 FUEL FILTER BYPASS INDICATION LIGHTS CAME ON AND STAYED ON, CREW ELECTED TO TERMINATE FLIGHT, DUMPED 156,000 LBS OF FUEL, RETURNED TO KJFK AND LANDED SAFELY. AFTER LANDING MAINTENANCE CREW IN KJFK REPLA
- [SDR Q2SA758006](https://openairdocs.org/sdr/Q2SA758006.md): Slide · unwanted deploy · Apr 20, 2009 · N758SA · Boeing 747281F · Escape Slide
  > PRIOR TO DEPARTURE FROM KJFK, LEFT UPPER DECK EMERGENCY EXIT SLIDE INADVERTENTLY DEPLOYED. REMOVED SLIDE IN ACCORDANCE WITH AMM 25-68-02. TRANSFERRED TO DEFERRED MAINTENANCE ITEM NR 18844 PER MEL 25-11, CAT. C. PLACARD INSTALLED.
- [SDR Q2SA758005](https://openairdocs.org/sdr/Q2SA758005.md): Pms · inactive · Mar 17, 2009 · N758SA · Boeing 747281F · Flight Management Computing Hardware System
  > CLIMB-OUT OF EBLG, PERFORMANCE MANAGEMENT SYSTEM (PMS) LIGHT ILLUMINATED IN FLIGHT AND AUTOPILOTS "A" AND "B" WOULD NOT FOLLOW FLIGHT MANAGEMENT SYSTEM (FMS) COMMAND. AIR TURN BACK TO EBLG. NO FUEL DUMPED. OPERATIONALLY CHECKED IN ACCORDANCE WITH DELCO OPER
- [SDR Q2SA758004](https://openairdocs.org/sdr/Q2SA758004.md): Thrust Reverser · deployed · Dec 21, 2008 · N758SA · Boeing 747281F · Engine Thrust Reverser
  > ON CLIMB-OUT FROM ADDIS ABABA, ETHIOPIA (HAAB), AIRCRAFT PERFORMED AN AIR TURN BACK DUE TO INDICATION OF NR 4 ENGINE THRUST REVERSER TRYING TO DEPLOY IN FLIGHT. CREW WAS ALERTED BY THRUST REVERSER VALVE LIGHT AND TRANSIT LIGHT ILLUMINATING. CREW RETURNED TO
- [SDR Q2SA783002](https://openairdocs.org/sdr/Q2SA783002.md): Pitot Line · broken · Dec 15, 2008 · N783SA · Boeing 747281F · Pitot/Static System
  > ON DEPARTURE FROM KJFK, CAPTAIN'S POSITION LOST ALL PRIMARY INSTRUMENTS (AIRSPEED, ALTITUDE, IVSI INDICATORS). AIR TURN BACK TO KFJK, NO FUEL DUMP PERFORMED. CADC REPLACED AND BROKEN PITOT LINE FOUND BEHIND CAPTAIN'S ALTIMETER.
- [SDR Q2SA758003](https://openairdocs.org/sdr/Q2SA758003.md): Engine · damaged · Oct 9, 2008 · N758SA · Boeing 747281F · Engine (Turbine/Turboprop)
  > DURING TAKEOFF AFTER V1 FROM HAAB, BIRD INGESTION INTO NR 3 ENGINE. AIR TURNBACK TO HAAB. FUEL DUMP OF 50,000 LBS. INSPECTION AFTER LANDING CONFIRMED DAMAGE TO NR 3 ENGINE FAN BLADES, AS WELL AS EVIDENCE OF BIRD STRIKE ON NR 2 ENGINE. NR 1, 3, 4, 6, 11, 13

Next page: https://openairdocs.org/model/boeing-747-281f/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 = '747281F'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-747-281f/reports

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