# Service difficulty reports: N942UP, cancelled Dec 4, 2007

A list on [N942UP, cancelled Dec 4, 2007](https://openairdocs.org/deregistered/N942UP-2007-12-04.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 4 · 172 reports

- [SDR UPS07249849](https://openairdocs.org/sdr/UPS07249849.md): Battery Pack · inoperative · May 23, 2007 · N942UP · Boeing 72722C · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT OVER CABIN ENTRY DOOR INOP. REMOVED AND REPLACED BATTERIES IN EMERGENCY EXIT LIGHT IAW B727 MM 33-50-67-2. OPS CHECKS NORMAL.
- [SDR UPS06248018](https://openairdocs.org/sdr/UPS06248018.md): Actuator · worn · Sep 21, 2006 · N942UP · Boeing 72722C · Leading Edge Slat Actuator
  > LED NR 6 DOES NOT RETRACT. THE AMBER LT CAME ON DURING CLIMB TO 310. COULD NOT DUPLICATE FAULT ON GROUND. AS PRECAUTION REPLACED NR 6 L/E SLAT ACTUATOR. OPS CHECK GOOD, REF MM 27-81-32-4.
- [SDR 2007FA0000197](https://openairdocs.org/sdr/2007FA0000197.md): Ring · elongated · Sep 4, 2006 · N942UP · Boeing 72722C · Escape Slide
  > DURING ROUTINE C-CHECK INSPECTION OF FORWARD DOOR EMERGENCY ESCAPE SLIDE, THE SLIDE BUSTLE LATCH CHAIN WAS FOUND DETACHED FROM THE SPLIT RING. THE SPLIT RING HAD BECOME ELONGATED AND THE RING COILS HAD SEPARATED THUS ALLOWING THE CHAIN TO DETACH. THE SLIDE W
- [SDR UPS06247858](https://openairdocs.org/sdr/UPS06247858.md): Hinge · cracked · Aug 24, 2006 · N942UP · Boeing 72722C · Ailerons
  > INSPECTION TYPE:C CRACK FOUND AFT FASTENER HOLE OF LT O/B AILERON 2ND FROM I/B FIXED W WING HINGE CASTING UPPER O/B FLANGE. REPLACE HINGE ASSY. HINGE ASSY REPLACED IAW SRM 51-30-2, 51-30-5 AND MM 27-10-14, 21-80-01 AND BOEING DRAWING 65-19275. REF NRC 10080
- [SDR UPS06247849](https://openairdocs.org/sdr/UPS06247849.md): Fairing · corroded · Aug 18, 2006 · N942UP · Boeing 72722C · Aerodynamic Fairings
  > INSPECTION TYPE:C BODY FAIRING 3430 HAS AREA OF LIGHT SURFACE CORROSION LWR DOOR CUTOUT FRAME. PLEASE REMOVE ANCHOR NUTS, REMOVE CORROSION, REINSPECT AND RECTIFY AS NECESSARY. FRAME AND SUPPORT BRACKET REPAIRED IAW SRM 51-40-04 AND 51-30-02.
- [SDR UPS06247815](https://openairdocs.org/sdr/UPS06247815.md): Bushing · corroded · Aug 15, 2006 · N942UP · Boeing 72722C · Engine Mount Section
  > INSPECTION TYPE: C ENGINE NR 3 FWD MOUNT FITTING HAS PITTING CORROSION ON REPAIR BUSHING IN AFT OB HOLE FITTING REPAIR BUSHING REMOVED IAW SOPM 20-50-03. REPAIR CARRIED OUT IAW APPX B.
- [SDR UPS06247804](https://openairdocs.org/sdr/UPS06247804.md): Bracket · cracked · Aug 15, 2006 · N942UP · Boeing 72722C · Fuselage Main, Structure
  > INSPECTION TYPE:C SUSPECT CRACK IN 870 BULKHEAD O/B OF LT 870 FITTING AT LWR CORNER, CRACK IDENTIFIED ON BRACKET REMOVED BRACKET IAW SRM 51-30-02. NEW BRACKET INSTALLED IAW SRM 51-30-02 AND DRAWING NR 65-25370.
- [SDR UPS06247806](https://openairdocs.org/sdr/UPS06247806.md): Skin · scratched · Aug 14, 2006 · N942UP · Boeing 72722C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C SCRATCH ON FUSELAGE SKIN BETWEEN BS 1186 AND 1193 S19R. PAINTSTRIP AREA A RE-INSPECT AND RECTIFY AREA PAINT STRIPPED IAW MM 51-20-01. SCRATCH OUTSIDE LIMITS IAW SRM 5 3-30-1. REPAIR CARRIED OUT IAW SRM 53-30-03 AND 51-30-02.
- [SDR UPS06247897](https://openairdocs.org/sdr/UPS06247897.md): Ring · broken · Aug 11, 2006 · N942UP · Boeing 72722C · Escape Slide
  > INSPECTION TYPE-C ON SLIDE LATCH CHAIN AND RING BROKEN ON FWD ENTRY DOOR ESCAPE SLIDE. REPLACE RING AND CHAIN ON FURTHER INVESTIGATION CHAIN FOUND NOT TO BE BROKEN, BUT RING WAS DEFORMED AND DETACHED. RING REPLACED IAW MM 25-60-14. NOTE: RING SOLDERED W/NO D
- [SDR UPS06247831](https://openairdocs.org/sdr/UPS06247831.md): Skin · cracked · Aug 11, 2006 · N942UP · Boeing 72722C · Trailing Edge Flaps
  > INSPECTION TYPE-C CRACK ON RT OB FORE FLAP LE AT CUTOUT OB OF IB SEQUENCE CARRIAGE ATTACH BRACKET DAMAGE OUTSIDE LIMITS IAW SRM 57-50-1. CRACK STOP DRILLED IAW SRM 57-5 0-4. HFEC CARRIED OUT IAW NDTM 51-00-00 PT 6 FIG 4 CRACK CONTAINE D. REPAIR CARRIED OUT I
- [SDR UPS06247830](https://openairdocs.org/sdr/UPS06247830.md): Support · cracked · Aug 10, 2006 · N942UP · Boeing 72722C · Nacelle/Pylon Miscellaneous Structure
  > INSPECTION TYPE-C ENGINE NR 2 SUPPORT STRUCTURE ABOVE HORIZONTAL FIREWALL HAS SUSPECT CRACK ON RT CHORD BETWEEN AFT CONE BOLT HOUSING AND REAR SPAR AT 2 FOOT FROM TOP OF CHORD HFEC CARRIED OUT IAW NDTM 51-00-00 PT6 FIG 4. CRACK CONFIRMED. CHORD REPLACED IAW DR
- [SDR UPS06247823](https://openairdocs.org/sdr/UPS06247823.md): Floorbeam · corroded · Aug 9, 2006 · N942UP · Boeing 72722C · Fuselage Main, Floor Beam
  > INSPECTION TYPE-C CORROSION AT BS 344 OUTSIDE LIMITS, PLEASE REPAIR IAW SRM FLOORBEAM TOP CHORD REMOVED IAW SRM 51-30-02. SPLICE ANGLES AND TOP CHORD FABRICATED IAW SRM 53-10-08. PARTS REPROTECTED IAW SRM 51-10-02. PARTS INSTALLED IAW SRM 51-30-02.
- [SDR UPS06247745](https://openairdocs.org/sdr/UPS06247745.md): Floorbeam · corroded · Aug 9, 2006 · N942UP · Boeing 72722C · Fuselage Main, Floor Beam
  > INSPECTION TYPE: C, ON REMOVAL OF FLOOR PANEL AT ENTRANCE TO COCKPIT. CORROSION FOUND ON FLOORBEAM TOP CAP BS 344 LBL 10 TO RBL 12. AREA FOUND TO BE OUTSIDE LIMITS IAW SRM 53-10-1.
- [SDR UPS06247721](https://openairdocs.org/sdr/UPS06247721.md): Pressure Panel · cracked · Aug 8, 2006 · N942UP · Boeing 72722C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C SUSPECT CRACK ON NLG SIDE WALL AT WL 184 BS 276. CRACK REPAIRED IAW SRM 51-40-02.
- [SDR UPS06247746](https://openairdocs.org/sdr/UPS06247746.md): Pressure Panel · cracked · Jul 26, 2006 · N942UP · Boeing 72722C · Fuselage Main, Bulkhead
  > INSPECTION TYPE: C, DURING PRESSURIZATION CHECK LEAK WAS FOUND IN NOSE WW PRESSURE DECK CE CEILING. WEB CRACKED. REPAIR CARRIED OUT IAW SRM 51-30-02, 51-40-02, 51-10-02 & 51-10-01.
- [SDR UPS06246886](https://openairdocs.org/sdr/UPS06246886.md): Light · inoperative · May 17, 2006 · N942UP · Boeing 72722C · Emergency Lighting
  > INSPECTION TYPE:ASE FLIGHT STAT EMERGENCY LIGHT INOP. REMOVED & REPLACED EMERGENCY EXIT LIGHT ASSY IAW 33-50-01-2. OPS CHECK GOOD.
- [SDR UPS06247805](https://openairdocs.org/sdr/UPS06247805.md): Bracket · cracked · May 8, 2006 · N942UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C SUSPECT CRACK IN 870 BULKHEAD O/B OF RT 870 FITTING AT LWR CORNER. CRACK IDENTIFIED ON BRACKET, REMOVED BRACKET IAW SRM 51-30-02. NEW BR BRACKET INSTALLED IAW SRM 51-30-02 AND DRAWING NR 65-25370.
- [SDR UPS05244165](https://openairdocs.org/sdr/UPS05244165.md): Skin · corroded · Mar 15, 2005 · N942UP · Boeing 72722C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C AREAS OF LITE SURFACE CORROSION FOUND ON INNER FUSELAGE SKIN SURFACE OF LWR SURFACE OF INTERNAL DOUBLER BETWEEN S3L & S2L BS 630 TO 660 AT VARIOUS LOCATIONS. REPAIR CARRIED OUT IAW SRM 53-30-03.
- [SDR UPS05244169](https://openairdocs.org/sdr/UPS05244169.md): Fitting · cracked · Mar 11, 2005 · N942UP · Boeing 72722C · Wing, Attach Fittings
  > INSPECTION TYPE:C EXTENSIVE CRACKING SROUND BOTH I/B B & C HOLES FOR A LARGE AREA OF THE RT TRUNNION FITTING ON RT REAR SPAR. REMOVED MLG FWD TRUNNION HOUSING ATTACHMENT FITTING ON REAR SPAR IAW SRM 51-30-2. REPAIR CARRIED OUT IAW SRM 51-30-2, DRAWING 65-192
- [SDR UPS05244134](https://openairdocs.org/sdr/UPS05244134.md): Bracket · cracked · Mar 11, 2005 · N942UP · Boeing 72722C · Engine Thrust Reverser
  > INSPECTION TYPE:C ENGINE NR 1 THRUST REVERSER O/B FAIRING MID AND AFT SUPPORT BRACKET ARE CRACKED. BRACKETS REPLACED IAW MM 78-30-01.
- [SDR UPS05244172](https://openairdocs.org/sdr/UPS05244172.md): Fitting · corroded · Mar 10, 2005 · N942UP · Boeing 72722C · Trailing Edge Flaps
  > INSPECTION TYPE:C NR 5 FLAP TRACK FWD SUPPORT FITTING P/N 65-21651 HAS PITTING CORROSION ON HOLE FOR SPECIAL STUD. REPAIR CARRIED OUT IAW AAAE EO 2005-021-003.
- [SDR UPS05244166](https://openairdocs.org/sdr/UPS05244166.md): Cargo Track · cracked · Mar 10, 2005 · N942UP · Boeing 72722C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C CARGO TIE DOWN TRACK CRACKED AT BS 1030 RBL 14. REPAIR CARRIED OUT IAW SRM 53-10-5, 51-30-2, 51-20-1 & 53-10-5.
- [SDR UPS05244146](https://openairdocs.org/sdr/UPS05244146.md): Floor Support · cracked · Mar 10, 2005 · N942UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C FLOOR SUPPORT CRACKED AT BS 1070 LBL 14. REPLACED FLOOR SUPPORT FROM 1100 - 1060 IAW SRM 53-10-5 FIG 4.
- [SDR UPS05244167](https://openairdocs.org/sdr/UPS05244167.md): Skin · cracked · Mar 9, 2005 · N942UP · Boeing 72722C · Cargo/Baggage Doors
  > INSPECTION TYPE: C FWD CARGO DOOR CRACKED AT AFT UPPER FRAME BETWEEN LWR ATTACH BOLT FOR BALANCE MECHANISM. REPAIR CARRIED OUT IAW AAAE EO 2005-021-002.
- [SDR UPS05244154](https://openairdocs.org/sdr/UPS05244154.md): Spindle · corroded · Mar 9, 2005 · N942UP · Boeing 72722C · Trailing Edge Flap Control System
  > INSPECTION TYPE:C SURFACE CORROSION ON 4 FLAP CARRIAGE SPINDLE INNER SURFACE. CORROSION REMOVED IAW SRM 51-00-06, WITHIN LIMITS OHM 57-52-01. AREA PROTECTED IAW SRM 51-10-02.
- [SDR UPS05244151](https://openairdocs.org/sdr/UPS05244151.md): Channel · cracked · Mar 9, 2005 · N942UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C UPPER SUPPORT CHANNEL FOR EQUIPMENT RACK CRACKED AT BS 420 AND 460 RBL 22. REPAIRED CRACKED UPPER SUPPORT CHANNEL IAW SRM 51-90-3 AT BS 420 TO 460.
- [SDR UPS05244148](https://openairdocs.org/sdr/UPS05244148.md): Channel · cracked · Mar 9, 2005 · N942UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C UPPER SUPPORT CHANNEL FOR EQUIP RACK CRACKED AT BS 400 BS 420 AND BS 460 LBL 17. REPAIRED CRACKS ON UPPER SUPPORT CHANNEL AT BS 400, 420, 460 LBL 17 IAW SRM 51-40-3.
- [SDR UPS05244170](https://openairdocs.org/sdr/UPS05244170.md): Tab · delaminated · Mar 8, 2005 · N942UP · Boeing 72722C · Elevator, Tab Structure
  > INSPECTION TYPE:C EVIDENCE OF DELAMINATION TO RT ELEVATOR TAB UPPER INBOARD SURFACE. TAB REPLACED IAW MM 27-30-11 & 27-30-00.
- [SDR UPS05244168](https://openairdocs.org/sdr/UPS05244168.md): Panel · delaminated · Mar 8, 2005 · N942UP · Boeing 72722C · Spoilers
  > INSPECTION TYPE:C DELAMINATION ON NR 8 SPOILER AT I/B END. NR 8 SPOILER PANEL REPLACED IAW MM 27-62-01 AND SPOILER LINK REPLACED IAW MM 27-62-91.
- [SDR UPS05244135](https://openairdocs.org/sdr/UPS05244135.md): Frame · cracked · Mar 8, 2005 · N942UP · Boeing 72722C · Cargo/Baggage Doors
  > INSPECTION TYPE:C AFT CARGO DOOR, CRACKED IN 1ST FRAME FROM TOP IN O/B RADIUS BENEATH FWD HINGE. REPAIR CARRIED OUT IAW MM 52-31-01 & SRM 51-10-01, 51-40-3, 51-10-02 & 51-30-02. REF NRC 768566 FOR INSTALLATION OF AFT CARGO DOOR.
- [SDR UPS05243938](https://openairdocs.org/sdr/UPS05243938.md): Life Raft · malfunctioned · Feb 22, 2005 · N942UP · Boeing 72722C · Life Raft
  > LIFE RAFT LOCATED AFT OF LAV EXPERIENCED AN UNCOMMANDED INFLATION. NO DAMAGE TO THE A/C WAS NOTICED. A/C NOW IN HEAVY MAINTENANCE IN SNN. INSTALLED SERVICEABLE LIFE RAFT MM 25-60-00 LOG PAGE 333531 THIS WAS TRANSFERRED TO NRC768041 AT SNN.
- [SDR UPS04241937](https://openairdocs.org/sdr/UPS04241937.md): Skin · damaged · Feb 6, 2004 · N942UP · Boeing 72722C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C PARTIAL REPLACEMENT OF SKIN LOCATED AT BS 360-390 S4L-4R. REPLACED IAW UPS AUTHORIZATION B727-5330-19967-A.
- [SDR UPS04241932](https://openairdocs.org/sdr/UPS04241932.md): Rib · cracked · Feb 4, 2004 · N942UP · Boeing 72722C · Wing, Rib/Bulkhead
  > INSPECTION TYPE:C ON REMOVAL OF PANEL 8855 FOUND NR 14 O/B SPOILER DOWN STOP RIB CRACKED AT WS 620.5. CRACKED RIB REPLACED IAW SRM 51-30-2 & SPOILER OPERATION WITH STOP TESTED SATISFACTORY IAW MM 27-61-00.
- [SDR UPS04241875](https://openairdocs.org/sdr/UPS04241875.md): Bracket · cracked · Feb 2, 2004 · N942UP · Boeing 72722C · Battery Box Structure
  > INSPECTION TYPE: C, BATTERY CHARGER FWD MOUNTING BRACKET CRACKED ON E3 RACK LOWER RT SIDE. REMOVED CRACKED BRACKET IAW SRM 51-30-02. FABRICATED NEW BRACKET IAW SRM 51-20-01. NEW BRACKET REPROTECTED IAW SRM 51-10-02, AND RE-INSTALLED IAW SRM 51-30-02.
- [SDR UPS04241872](https://openairdocs.org/sdr/UPS04241872.md): Bracket · damaged · Jan 30, 2004 · N942UP · Boeing 72722C · Aerodynamic Fairings
  > INSPECTION TYPE: C, LATCH FITTING ON W/BODY FAIRING BRACKET FOR AFT CARGO DOOR FAIRING LATCH IS DAMAGED. BRACKET REPLACED IAW SRM 51-20-01.
- [SDR UPS04241876](https://openairdocs.org/sdr/UPS04241876.md): Bracket · corroded · Jan 25, 2004 · N942UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C, SUSPECT CORROSION WHERE 259.5 RT STIFFENER AND TOP LEFT HAND CORNER OF NWW TORQUE BOX MEET BRACKET. REMOVED IAW SRM 51-30-02. BRACKET FABRICATED IAW SRM 51-20-01. FASTENERS INSTALLED IAW SRM 51-30-2 & APPLIED SEALANT IAW SRM 51-20-04. B
- [SDR UPS04241898](https://openairdocs.org/sdr/UPS04241898.md): Web · cracked · Jan 23, 2004 · N942UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C, AFT STAIRWELL RT TORQUE BOX VERTICAL WEB HAS CRACKING BEYOND PREVIOUS REPAIR AT BS 1273. REPAIR CARRIED OUT IAW EO B727-5310-1239-E & MM 20-10-05.
- [SDR UPS04241873](https://openairdocs.org/sdr/UPS04241873.md): Hinge · cracked · Jan 23, 2004 · N942UP · Boeing 72722C · Landing Gear Doors
  > INSPECTION TYPE: C, LEFT WING GEAR DOOR AFT HINGE, INNER HINGE HALF CRACKED. REPLACED HINGE IAW SRM 51-30-02.
- [SDR UPS04241940](https://openairdocs.org/sdr/UPS04241940.md): Beam · corroded · Jan 22, 2004 · N942UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C PRESENCE OF INTERGRANULAR CORROSION FOUND ON VARIOUS HOLES AND THE LOWER I-BEAM AT BS 1110 RBL 31 AS MARKED. REPAIRED IAW UPS AUTHORIZATION B727-53-21034.
- [SDR UPS04241933](https://openairdocs.org/sdr/UPS04241933.md): Support Fitting · damaged · Jan 22, 2004 · N942UP · Boeing 72722C · Spoilers
  > INSPECTION TYPE:C REPAIR PLATES ON NR 3 SPOILER PCU SUPPORT FITTING, REAR SPAR ATTACH ANGLES DO NOT CONFORM TO REQUIREMENTS OF SRM REPAIR 51-40-4 FIG 1 OR S/B 57-84 R1 CRITERIA. REPAIR CARRIED OUT IAW DRAWING 65-16201 & MM 28-11-20 & 28-11-21.
- [SDR UPS04241816](https://openairdocs.org/sdr/UPS04241816.md): Bracket · corroded · Jan 22, 2004 · N942UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C, INTERGRANULAR CORROSION FOUND ON CEILING PANEL BRACKET AT BS 1130 AFT CARGO COMPT, AS MARKED. HFEC INSPECTION CARRIED OUT AROUND CUTOUT AT THE ABOVE AREA IAW B727 NDTM PT 6 51-00-00 NDF. REPAIR CARRIED OUT IAW SRM 51-40-04.
- [SDR UPS04241939](https://openairdocs.org/sdr/UPS04241939.md): Fitting · cracked · Jan 21, 2004 · N942UP · Boeing 72722C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C RIGHT MLG WHEEL WELL, EVIDENCE OF CORROSION ON BS 870 FITTING O/B FLANGE AREA ABOVE STR 18A. FITTING REPLACED IAW DWG65C23231 AND 2BOF65-72710 AND UPS EO B727-5310-3056G.
- [SDR UPS04241874](https://openairdocs.org/sdr/UPS04241874.md): Solenoid Valve · sticking · Jan 21, 2004 · N942UP · Boeing 72722C · Fire Bottle, Fixed
  > INSPECTION TYPE: C, ENGINE NR 1 FIRE EXTINGUISHING SOLENOID STICKS DURING OPERATION. ENGINE NR 1 FIRE SOLENOID VALVE REPLACED IAW MM 26-21-21. TEST AND FOUND SATISFACTORY IAW MM 21-21-00.
- [SDR UPS02238739](https://openairdocs.org/sdr/UPS02238739.md): Carriage · corroded · Jul 8, 2002 · N942UP · Boeing 72722C · Trailing Edge Flaps
  > INSPECTION TYPE:C+SI FLAP CARRIAGE NR 1 HAS SUSPECT CORROSION INSIDE SPINDLE BORE. REMOVAL OF HARDWARE CORROSION FOUND ON SPINDLE SMALL BEARING SEAT. CORROSION FOUND TO BE OUTSIDE LIMITS OF OHM 57-58-01. FLAP CARRIAGE REPLACED IAW MM27-51-13.
- [SDR UPS02238849](https://openairdocs.org/sdr/UPS02238849.md): Fitting · cracked · Jul 1, 2002 · N942UP · Boeing 72722C · Fuselage, Landing Gear Attach Fittings
  > INSPECTION TYPE:C+SI DURING RECTIFICATION UPPER LT AFT TENSION TIE FITTING FOUND CRACKED IN TAIL SKID UNIT CAVITY. UPPER LT TENSION TIE REMOVED IAW SRM 51-30-02 UPPER LT TENSION TIE INSTALLED IAW 51-30-02.
- [SDR UPS02238844](https://openairdocs.org/sdr/UPS02238844.md): Door Frame · cracked · Jun 27, 2002 · N942UP · Boeing 72722C · Cargo/Baggage Doors
  > INSPECTION TYPE:C+SI SUSPECT CRACKS ON 2 FRAMES AND FRAME ATTACH ANGLES ON OUTER FACE OF AFT CARGO DOOR. FRAMES AND ANGLES REPLACED IAW DWG 65-18625, LOWER FRAME REPAIRED IAW SRM 51-40-2 FIG 1.
- [SDR UPS02238804](https://openairdocs.org/sdr/UPS02238804.md): Stringer · cracked · Jun 21, 2002 · N942UP · Boeing 72722C · Fuselage Main, Structure
  > INSPECTION TYPE:C+SI STR NO8 L/H HAS EVIDENCE OF CRACKING ON ROOT OF INSIDE LOWER FLANGE AT BS 460 REPAIR CARRIED OUT IAW SRM 53-10-3 FIGURE 3.
- [SDR UPS02238786](https://openairdocs.org/sdr/UPS02238786.md): Hinge · corroded · Jun 21, 2002 · N942UP · Boeing 72722C · Cargo/Baggage Doors
  > INSPECTION TYPE:C+SI SEVERAL MAIN HINGES CORRODED ON MAIN CARGO DOOR. HINGES REPLACED IAW OHM 20-50-01.
- [SDR UPS02238851](https://openairdocs.org/sdr/UPS02238851.md): Intercostal · cracked · Jun 20, 2002 · N942UP · Boeing 72722C · Fuselage Main, Structure
  > INSPECTION TYPE:C+SI BS 950 LBL 6 ANGLE CRACKED AT FLOOR BEAM INTERCOSTEL. NEW ANGLE FABRICATED IAW SRM 51-20-1 FIG.7 ANGLE INSTALLED IAW SRM 51-30-2.
- [SDR UPS02238830](https://openairdocs.org/sdr/UPS02238830.md): Doubler · corroded · Jun 20, 2002 · N942UP · Boeing 72722C · Fuselage Main, Structure
  > INSPECTION TYPE:C+SI BULGING ON EXTERNAL DOUBLER ATTACHED TO DELTA BEAM BS 747 Y/H DOUBLER REMOVED IAW SRM 51-30-2, CORROSION FOUND ON UDERSIDE OF DOUB LER, DELTA BEAM FAYING SURFACE INSPECTED AND LIGHT SURFACE CORROSION FOUND, REMOVED AND FOUND WITHIN LI

Next page: https://openairdocs.org/deregistered/N942UP-2007-12-04/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 = 'N942UP' AND deregistration_id = 'N942UP-2007-12-04'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N942UP-2007-12-04/reports

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